Publications
 2017  2016  2015  2014  2013  2012  2011  2010  2009  2008  2007  2006  2005  2004  2003  2002  2001  2000 
 1999  1998  1997  1996  1995  1994  1993  1992  1991  1990  1989  1988  1987  1986  1985  1984  1983  1982 
 1981  1980  1979  1978  1977  1976  1975  1974  1973  1972  1971  1970  1969  1968  1967  1966  1965  1964 
2017 (back to top)
 Anderson, W.K., Newman III, J.C., and Karman, S.L., “Stabilized Finite Elements in FUN3D,” AIAA Science and Technology Forum and Exposition, AIAA Paper 20170077, Grapevine, TX, January 2017.
 J. Cho, Z. Hu, N. Fell, G. Heath, R. Qayyum, and M. Sartipi, “Hospital Discharge Disposition of Stroke Patients in the State of Tennessee,” Revised and resubmitted to the Journal of the Southern Medical Association, January 2017 .
 B. Williams, B. Allen, Z. Hu, H. True, J. Cho, A. Harris, N. Fell, and M. Sartipi, "RealTime Fall Risk Assessment Using Functional Reach Test," The International Journal of Telemedicine and Applications, January 2017.
 Hereth, E., Sreenivas, K., Taylor, L.K., and Nichols, D.S., "An Automatic Parallel
Octree Grid Generation Software with an Extensible Solver Framework and a Focus on
Urban Simulation" AIAA Paper 20170587, Grapevine, TX, January 2017.
http://arc.aiaa.org/doi/abs/10.2514/6.20170587  Guven E, Parnell LA, Jackson ED, Parker MC, Gupta N, Rodrigues J, Qin H., "Hydrogen peroxide induced loss of heterozygosity correlates with replicative lifespan and mitotic asymmetry in Saccharomyces cerevisiae," PeerJ. 2016;4:e2671. doi: 10.7717/peerj.2671. PubMed PMID: 27833823; PMCID: 5101604.
 Liu, T., Hilbert, C.B., Lin, W., and Hereth, E.A., "Automatic highorder mesh generation with SpringField and vectoradding: 3D domain mesh generation extension I," 55th AIAA Aerospace Sciences Meeting, Grapevine, Texas, January 2017.
2016 (back to top)
 Collao, M.D., Webster, R.S., Sreenivas, K., and Lin, W., "Computational Study of the Effects of Protruding Studs Casing Treatment on the Performance of an Axial Transonic Turbofan, " AIAA Paper 20164646, 52nd AIAA/SAE/ASEE Joint Propulsion Conference, 2016, 10.2514/6.20164646.
 Lin, W., Newman III, J.C., and Anderson, W.K., “Design of Broadband Acoustic Cloak using Topology Optimization,” Accepted for publication, ASME International Mechanical Engineering Congress & Exposition, IMECE Paper 201668135, Phoenix, AZ, Nov. 2016.
 A. Harris, H. True, Z. Hu, J. Cho, N. Fell, and M. Sartipi, “Fall Recognition using Wearable Technologies and Machine Learning Algorithms,” the Proc. of IEEE Big Data Conference, December 2016.
 Mittal, A., Briley, R., Sreenivas, K., and Taylor, L.K., "A Parabolic VelocityDecomposition Method for Wind Turbines," Journal of Computational Physics, Available online 19 October, 2016.
 Mittal, A., Sreenivas, K., Taylor, L., Hereth, L., Hilbert, C.B., “BladeResolved Simulations of a Model Wind Turbine: Effect of Temporal Convergence,” Wind Energy, Volume 19, Issue 10, pp 17611783, October 2016.
 Liu, Tuo, Hilbert, C. Bruce , “Highorder mesh movement with SpringField and vectoradding,” Research Note, 25th International Meshing Roundtable, Sandia National Laboratories, September 2630 2016.
 Raoufi, A., Newman, J. C., Kapadia, S., "Computational optimization and sensitivity Analysis of methane fuel reformer," Computers & Chemical Engineering, 93, 266–28 (2016).

Raoufi, A., Kapadia, S., & Newman III, J. C., "Sensitivity Analysis and Computational Optimization of Fuel Reformer," ASME 2016 14th Fuel Cell Science, Engineering, and Technology Conference. Charlotte, NC (2016).

Raoufi, A., Kapadia, S., & Newman III, J. C., "Computational Simulation of Thermal and Chemical Phenomena for a HoneycombStructured Catalytic Reforming Reactor," 229th ECS meeting. San Diego, CA (2016).

Lin, W., Newman III, J.C., Anderson, W.K., Zhang, X., “Broadband Shape and Topology Optimization of Acoustic Metamaterials and Phononic Crystals,” AIAA Paper 20163216, 17th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, AIAA Aviation and Aeronautics Forum and Exposition 2016, Washington, D.C., 1317 June 2016.

Lin, W., Newman III, J.C., Anderson, W.K., Zhang, X., “Shape Optimization of Acoustic Metamaterials and Phononic Crystals with a TimeDependent Adjoint Formulation: ThreeDimensional Applications,” AIAA Paper 20163830, 17th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, AIAA Aviation and Aeronautics Forum and Exposition 2016, Washington, D.C., 1317 June 2016.

Ghasemi, A., Taylor, L.K. and Newman III, J.C., "Spectral/hp Hull: A Degree of Freedom Reducing Discontinuous Spectral Element Method for Conservation Laws with Application to Compressible Fluid Flow", To be presented at 46th AIAA Fluid Dynamics Conference, June 2016.

Ghasemi, A. and Taylor, L.K., "Preconditioning Large Scale Iterative Solution of Ax = b Using a Statistical Method with Application to MatrixFree Spectral Solution of Helmholtz Equation", Procedia Computer Science Volume 80, 2016, Pages 2266–2270.

Ghasemi, A., Taylor, L.K. and Newman III, J.C., "MASSIVELY PARALLEL CURVED SPECTRAL/FINITE ELEMENT MESH GENERATION OF INDUSTRIAL CAD GEOMETRIES IN TWO AND THREE DIMENSIONS", to be presented at ASME 2016 Fluids Engineering Division Summer Meeting paper number FEDSM20167600.

Azarnoosh, J., Sreenivas, K., Arabshahi, A., "CFD Investigation of Human Tidal Breathing Through Human Airway Geometry," Procedia Computer Science, Vol. 80, 2016, pp 965  976.

Hasbestan, J.J., Newman III, J.C., and Arabshahi, A., "Pleasingly Parallel Matrix Free Discontinuous LeastSquares Spectral Element Algorithm for Fluid Flow with Nonconformal Element Refinement," FEDSM20167510, to be presented at ASME 2016 Fluids Engineering Division Summer Meeting, Washington, DC, July 1014, 2016.

Sreenivas, K., Mittal, A., Hereth, L., Taylor, L.K., and Hilbert, C.B., “Numerical Simulation of the Interaction Between Wind Turbines,” Journal of Wind Engineering and Industrial Aerodynamics, Vol. 157, pp. 145157, October 2016.

Azarnoosh, J., Sreenivas, K., Arabshahi, A., “CFD Investigation of Human Tidal Breathing through Human Airway Geometry,” International Conference on Computational Science (ICCS), San Diego, California, June 68, 2016.

Sreenivas, K, Webster, R.S., Hereth, E., Key, N.L., and Berdanier, R.A., “Computational Simulations of a Multistage Subsonic Research Compressor,” AIAA Paper 20160395, 54th AIAA Aerospace Sciences Meeting, January, 2016.

Liu, T., Wang, L., Karman, S.L., and Hilbert, B., “Automatic 2D highorder viscous mesh generation by SpringField and vectoradding,” AIAA Paper 20161673, 54th AIAA Aerospace Sciences Meeting, January, 2016.

Hasbestan, J.J., Newman III, J.C., and Arabshahi, A., “Least Squares Spectral Element Method For Laminar Compressible Flows,” AIAA Paper 20161075, 54th AIAA Aerospace Sciences Meeting. January, 2016.

Lin, W., Anderson, W.K., Newman III, J.C., and Zhang, X., “Shape Optimization of TwoDimensional Acoustic Metamaterials and Phononic Crystals with a TimeDependent Adjoint Formulation,” AIAA Paper 20161908, 57th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, January, 2016.

Mittal, A., Sreenivas, K., Briley, W.R., Taylor, L.K., “Towards Wind Farm Layout Design Using Sensitivity Derivatives Obtained from a Parabolic Method,” AIAA Paper 20162198, 34th Wind Energy Symposium, January, 2016.

Sreenivas, K., Mittal, A., Taylor, L.K., and Hereth, L., “HigherOrder Accurate Simulations of Wind Turbine Flow Fields: A Poor Man’s Approach,” AIAA Paper 20160749, 34th Wind Energy Symposium, January, 2016.
2015 (back to top)

Gruetzemacher, R., Arabshahi, A., and Pankajakshan, R., "Effects of Inhalation Transience on Particle Transport Through a CTBased Human Airway Geometry," IMECE201552606, International Mechanical Engineering Congress and Exhibition, Houston, TX, November 1319, 2015.

Mittal, A., Briley, W.R., Sreenivas, K., and Taylor, L.K., “A Parabolic VelocityDecomposition Method for Wind Turbines,” submitted to Journal of Computational Physics (under review), 2015.

Mittal, A., Briley, W.R., Taylor, L.K., and Sreenivas, K., “A Parabolic Method without Pressure Approximations for a Wind Farm,” EWEA Offshore 2015, Copenhagen: EWEA, 2015.

Liu, C., Newman III, J.C., and Anderson, W.K., "Petrov–Galerkin Overset Grid Scheme for the Navier–Stokes Equations with Moving Domains", AIAA Journal, Vol. 53, No. 11 (2015), pp. 33383353.

Gruetzemacher, R., Arabshahi, A., and Sreenivas, K., "Effects of Inhalation Transcience on Flow Structures During Numerical Simulation of Airflow through a CTBased Airway Geometry," Summer Biomechanics, Bioengineering and Biotransport Conference (SB3C), Snowbird Resort, Utah, June 1720, 2015.

Hassan, W.E., Sreenivas, K., Mittal, A., Taylor, L.K., and Hereth, L. "Blade Resolved Simulation for a Wind Farm," AIAA Paper 20152269, 33rd AIAA Applied Aerodynamics Conference, Dallas, TX, June 2015.

Mittal, A., Sreenivas, K., Briley, W.R., and Taylor, L.K., "A Parabolic Method for Accurate and Efficient Wind Farm Simulation," AIAA Paper 20152268, 33rd AIAA Applied Aerodynamics Conference, Dallas, TX, June 2015.

Mittal, A., Taylor, L.K., Sreenivas, K., Briley, W.R., and Nichols, D.S., "Extension of a Parabolic Method without Pressure Approximations for Wind Turbines in ABL Flows," AIAA Paper 20153391, 33rd AIAA Applied Aerodynamics Conference, Dallas, TX, June 2015.

Kamali, S., Ahrabi, B.R., Webster, R.S., and Sreenivas, K., "Numerical Simulation of Compressible Flow in a Diffusing Sduct with and without Vortex Generators," AIAA Paper 20152715, 33rd AIAA Applied Aerodynamics Conference, Dallas, TX, June 2015.

Karman, S. L., “AdaptiveOptimizationBased Smoothing for Tetrahedral Meshes,” AIAA20152038, SciTech 2015, Kissimmee, FL, January 2015.

Webster, R. S., Sreenivas, K., and Hilbert, C. B., “Computational Simulation of the Fan and Lowpressure Compressor Stages of the Energy Efficient Engine,” AIAA20151344, January, 2015.

Sreenivas, K., Mittal, A., Hereth, L., and Taylor, L.K., "Computational Simulation of the Interaction Between Tandem Wind Turbines with Offset," AIAA Paper 20150224, 33rd Wind Energy Symposium, AIAA SciTech 2015.

Mittal, A., Briley, W.R., Taylor, L.K., and Sreenivas, K., "A Parabolic Method without Pressure Approximations for Wind Turbines," AIAA Paper 20150728, 33rd Wind Energy Symposium, AIAA SciTech 2015.

Mittal, A., Sreenivas, K., Taylor, L.K., and Hereth, L., "Improvements to the Actuator Line Modeling for Wind Turbines," AIAA Paper 20150216, 33rd Wind Energy Symposium, AIAA SciTech 2015.
2014 (back to top)

Gruetzemacher, R., Abdollah Arabshahi, A., and Sreenivas, K.,"Numerical Simulation of Airflow in a CTbased Human Airway Model With Physiologically Appropriate Boundary Conditions," Poster Presentation within the Respiratory Bioengineering Track, Biomedical Engineering Society Annual Meeting, San Antonio, Texas, October 2014.

Hasbestan, J.J., Newman III, J.C., and Arabshahi,A.," A New Approach to Mesh Adaptation Procedure Using Linear Elasticity for Geometries Undergoing Large Displacements," FEDSM201422010, Proceedings of the ASME 2014 4th Joint USEuropean Fluids Engineering Division Summer Meeting and 11th International Conference on Nanochannels, Microchannels, and Minichannels, Chicago, Illinois, August 2014.

Ahrabi, B.R., Anderson, W.K., Newman III, J.C., "HighOrder FiniteElement Method and Dynamic Adaptation for TwoDimensional Laminar and Turbulent NavierStokes," 32nd AIAA Applied Aerodynamics Conference, June 2014, AIAA Paper 20142983.

Liu, C., Newman III, J.C., Anderson, W.K.," A Streamline/Upwind Petrov Galerkin Overset Grid Scheme for the NavierStokes Equations with Moving Domains," 32nd AIAA Applied Aerodynamics Conference, June 2014, AIAA Paper 20142980.

Wang, L., Anderson, W.K., Erwin, T. and Kapadia, S., "Discontinuous Galerkin and Petrov Galerkin Methods for Compressible Viscous Flows," Computers and Fluids, Vol. 100, pp. 1329.

Wang, L., Anderson, W.K., Kapadia, S. and Taylor, L.K., "Multiscale Large Eddy Simulation of Turbulence Using HighOrder Finite Element Methods," 7th AIAA Theoretical Fluids Mechanics Conference, Atlanta, GA, June 2014, AIAA Paper 20143211.

Sreenivas, K., Mittal, A., Hereth, L., Taylor, L.K., and Hilbert, C.B., “HighFidelity Computational Simulation of the Interaction between Tandem Wind Turbines,” 32nd AIAA Applied Aerodynamics Conference, June 2014, AIAA Paper 20142278.

Mittal, A., Sreenivas, K., Taylor, L.K., Hereth, L., Hilbert, C.B., and Hyams, D.G., “Investigation of Rotor Models for Wind Turbine Simulations,” 32nd AIAA Applied Aerodynamics Conference, Atlanta, GA, June 2014, AIAA Paper 20142280.

Gupta, A., Sreenivas, K., and Taylor, L.K., "Preconditioning Methods for Multiphase Flows," 11th AIAA/ASME Joint Thermophysics and Heat Transfer Conference, Atlanta, GA, June 2014, AIAA Paper 20142824.

Currier, N., and Sreenivas, K., "A Preconditioned NonSingular Eigensystem for the NavierStokes Equations with FiniteRate Chemistry," 7th AIAA Theoretical Fluids Mechanics Conference, Atlanta, GA, June 2013, AIAA Paper 20143084.

Mittal, A., Sreenivas, K., and Taylor, L.K., "Exploration of Modal Decomposition Techniques for Wind Turbines," AIAA20141398, SciTech 2014, National Harbor, MD, January 2014.

Karman, S. L., "MultiBlock Hierarchical Unstructured Grid Generation With Adaptation," AIAA20140116, SciTech 2014, National Harbor, MD, January 2014.

Currier, N., Franko, K., "A Discrete Error Transport Equation Source Model for Mesh Adaptation," AIAA20141431, 52nd AIAA Aerospace Sciences Meeting, National Harbor, MD, January 2014.
2013 (back to top)

Ahrabi, B.R., Sreenivas. K., and Webster, R.S., "Computational Investigation of Compressible Flow in a Diffusing Sduct," 49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference. San Jose, CA, July 2013, AIAA Paper 20133601.

Flynt, G.A., Webster, R.S., and Sreenivas. K., "Computation of Heat Transfer In Turbine Rotor Blade Cooling Channels with Angled Rib Turbulators," 49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference. San Jose, CA, July 2013, AIAA Paper 20133621.

Lin, W., Sreenivas, K., Webster, R.S., and Hyams, D.G., "Effect of Casing Groove Locations on the Performance of an Axial Flow Stage," 49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference. San Jose, CA, July 2013, AIAA Paper 20133632.

Sreenivas, K, Hilbert, C.B., Mittal, A., Hereth, L., and Taylor, L.K., "HighFidelity Computational Simulation of the Wake Characteristics of a Model Wind Turbine," 31st AIAA Applied Aerodynamics Conference, San Diego, CA, June 2013, AIAA Paper 20132416.

Erwin, T., Anderson, W.K., Kapadia, S. and Wang, L., “Three Dimensional Stabilized Finite Elements for Compressible NavierStokes”, AIAA Journal, 51(6), pp. 14041419, 2013.

Anderson, W.K., Wang, L., Newman, J. and Kapadia, S., “Extension of the Petrov Galerkin TimeDomain Algorithm for Dispersive Media”, IEEE Microwave And Components Letters, 23(5), pp. 234236, 2013.

Erwin, T., Anderson, W.K., Wang, L., and Kapadia, S., “Highorder Methods for Solutions of Threedimensional Turbulent NavierStokes”, AIAA 20132571, 21st AIAA Computational Fluid Dynamics Conference, June 2013.

Briley, W. Roger, "An Introduction to Vectors and Tensors from a Computational Perspective," Report UTCCECSSimCenter201301, May 3013.

Taylor, L.K., Sreenivas, K., Webster, R.S., and Kress, J., "An Artificial Compressibility Algorithm for Convective Heat Transfer," 44th AIAA Thermophysics Conference. June 2013, San Diego, CA, AIAA Paper 20132894.

Glasby, R., Burgess, N., Anderson, W.K., Wang, L., Allmaras, S. and Mavriplis, D., "Comparison of SU/PG and DG FiniteElement Techniques for the Compressible NaiverStokes Equations on Anisotropic Unstructured Meshes," AIAA paper 20130691, 51st AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, Dallas, TX, 0710 January, 2013.

O'Connell, M. and Karman Jr., S. L., "Mesh Rupturing: A Technique for Geometry Insertion and Significant Mesh Movement," AIAA Paper 20131048, 51st AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, Dallas, TX, 0710 January, 2013.

Wang, L., Anderson, W.K, Erwin, T., and Kapadia, S., "Highorder Methods for Solutions of Threedimensional Turbulent Flows," AIAA Paper 20130856, 51st AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, Dallas, TX, 0710 January, 2013.
2012 (back to top)

Mittal, A., and Taylor, L.K., "Optimization of Large Wind Farms Using a Genetic Algorithm," Proceedings of the ASME 2012 International Mechanical Engineering Congress & Exposition, Houston, TX, November 915, 2012.

Webster, R., Whitfield, D., Hilbert, B., Sreenivas, K., Hyams, D. and Briley, W., "Demonstration of Subsystem Level Simulations: A Coupled Inlet and Turbofan Stage," AIAA Paper 20124282, 48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Atlanta, GA, 2012.

Masters, J. S, Karman, S. L. Jr., “Manipulating Boundaries and Viscous Regions of Unstructured Meshes Using Winslow’s Equations”, AIAA Journal, Volume 50, Number 10, pp. 20802090, October 2012.

Wang, Li and Anderson, W. Kyle, “Shape Sensitivity Analysis for the Compressible NavierStokes Equations Via Discontinuous Galerkin Methods”, Computers & Fluids, Vol. 69, pp. 93107, 2012.

Ghasemi, A., Sreenivas, K., and Taylor, L.K., "Unconditionally stable highorder picard iteration algorithm for computational electromagnetics," IEEE Antennas and Propagation Society International Symposium (APSURSI), 8  14 July 2012 , Chicago, IL.

Wang, Li, Anderson, W. Kyle, Erwin, Taylor, and Kapadia, Sagar, “Solutions of Highorder Methods for Threedimensional Compressible Viscous Flows”, AIAA Paper 20122836, the 42nd AIAA Fluid Dynamics Conference, New Orleans, LA, June 2012.

Currier, N., Hyams, D., "A Hybrid Method for Flows in Local Chemical Equilibrium and Nonequilibrium", AIAA20121239, 50th AIAA Aerospace Sciences Meeting, Nashville, TN, January 2012.

Druyor Jr., C., Karman, S., "An Adaptive Hybrid Grid Generation Method for Complex Geometries", AIAA2012157, 50th AIAA Aerospace Sciences Meeting, Nashville, TN, January 2012.

O'Connell, M., Karman, S. "Techniques for Unstructured Mesh Adaptation with Elliptic Smoothing", AIAA2012156, 50th AIAA Aerospace Sciences Meeting, Nashville, TN, January 2012.

Lin, W., Sreenivas, K., Webster, R., Hyams, D.G., "Effect of Casing and Tip Modifications on the Performance of an Axial Flow Stage," AIAA Paper 20120475, 50th AIAA Aerospace Sciences Meeting, 9  12 January 2012, Nashville, TN.

Brock, W., Burdyshaw, C., Karman, S., Betro, V., Hilbert, B., Anderson, K., Haimes, R., "AdjointBased Design Optimization Using CAD Parameterization Through CAPRI", AIAA2012968, 50th AIAA Aerospace Sciences Meeting, Nashville, TN, January 2012.
2011 (back to top)

Mittal, A., Taylor, L.K., Sreenivas, K., and Arabshahi, A., “Investigation of Two Analytical Wake Models Using Data From Wind Farms,” Proceedings of the ASME 2011 International Mechanical Engineering Congress & Exposition, Denver, Co., November 1117, 2011.

Ghasemi, A., and Sreenivas, K., “On the Theory of a Novel HighOrder TimeMarching Algorithm Based on Picard Iteration,” UTCCECSSimCenter201102, September 2011.

Anderson, W. Kyle, Wang, Li, Kapadia, Sagar, Tanis, Craig, and Hilbert, Bruce, “PetrovGalerkin and discontinuous Galerkin methods for timedomain and frequencydomain electromagnetic simulations,” J. of Comp. Physics, Vol. 230, pp. 83608385, 2011. DOI: 10.1016/j.jcp.2011.06.025, Available online Sept. 15, 2011.

Arabshahi, A., Taylor, L.K., and Whitfield, D.L. “Computation of Dynamic Stability and Control Derivatives,” AIAA20113348, 29th AIAA Applied Aerodynamic Conference, Honolulu, Hawaii, June 2730, 2011.

Wang, L. and Anderson, W.K., “AdjointBased Shape Optimization for Electromagnetic Problems Using Discontinuous Galerkin Method,” AIAA Journal, Vol. 49, No. 6, pp 13021305, 2011.

Wang, L. and Anderson, W.K., “Sensitivity Analysis for the Compressible NavierStokes Equations Using A Discontinuous Galerkin Method,” AIAA20113408, 41st AIAA Fluid Dynamics Conference, June, 2011, Honolulu, Hawaii.

Hyams, D., Sreenivas, K., Webster, R., Currier, N., “A Generalized, Unstructured Interpolative Interface method for RotorStator Interactions,” AIAA20113700, 20th AIAA Computational Fluid Dynamics Conference, Honolulu, Hawaii, June 2730, 2011.

Erwin, J. Taylor, Anderson, W. Kyle, Wang, Li, and Kapadia, Sagar, “Three Dimensional Stabilized Finite Elements for Compressible NavierStokes,” 41st AIAA Fluid Dynamics Conference, June, 2011, Honolulu, Hawaii.

Nichols, III, D. S., “Accounting for Shocks in Turbulence Modeling,” 41st AIAA Fluid Dynamics Conference, June, 2011, Honolulu, Hawaii.

Epstein, J.M., Pankajakshan, R., Hammond, R.A., “Combining Computational Fluid Dynamics and AgentBased Modeling: A New Approach to Evacuation Planning,” PLoS ONE: Research Article, published 31 May 2011 10.1371/journal.pone.0020139.

Ji, L., “Unstructured Grid Technologies for Hydrodynamic Applications with Bodies in Relative Motion and Mesh Deformation,” PhD Dissertation, University of Tennessee at Chattanooga, April 2011.

Briley, W. R. and McDonald, H., “Reflections on the Evolution of Implicit Navier–Stokes Algorithms,” Computers & Fluids, 41:1519, 2011.

Pankajakshan, R., Mitchell, B.J., and Taylor, L.K., “Simulation of unsteady twophase flows using a parallel EulerianLagrangian approach,” Computers & Fluids, Volume 41, Issue 1, February 2011, Pages 2026.

Hyams, D.G., Sreenivas, K., Pankajakshan, R., Nichols, III, D.S., Briley, W.R., and Whitfield, D.L., “Computational simulation of model and full scale Class 8 trucks with drag reduction devices,” Computers & Fluids, Volume 41, Issue 1, February 2011, Pages 2740.

Karman, Jr., S.L., “Virtual Control Volumes for ThreeDimensional Unstructured Elliptic Smoothing,” AIAA2011893, 49th AIAA Aerospace Science Meeting, Orlando FL, January 2011.

Betro, V. and Karman, Jr., S.L., “Fully Anisotropic SplitTree Adaptive Refinement Mesh Generation Using Tetrahedral Mesh Stitching,” Proceedings of the 49th Annual AIAA Aerospace Sciences Meeting, Orlando, FL, January 47, 2011. AIAA20110895.

Kapadia, S., Anderson, W.K., and Burdyshaw, C., “Channel shape optimization of solid oxide fuel cells using advanced numerical techniques,” Computers & Fluids, Vol. 41, 2011, 4150.
2010 (back to top)

Masters, J. S., “Winslow Elliptic Smoothing Equations Extended to Apply to General Regions of an Unstructured Mesh,” PhD Dissertation, University of Tennessee at Chattanooga, December 2010.

Wang, L., Mavriplis, D.J., and Anderson, W.K., “Adjoint Sensitivity Formulation for Discontinuous Galerkin Discretizations in Unsteady Inviscid Flow Problems,” AIAA Journal, Vol. 48 (12), 2010.

Betro, V., “Implementing a NodeBased SplitTree Neighbor Search Algorithm,” Research Note, 19th Annual International Meshing Roundtable, Chattanooga, TN, October 68, 2010.

Karman, S.L. Jr., “Virtual Control Volumes for TwoDimensional Unstructured Elliptic Smoothing,” 19th International Meshing Roundtable, paper 2A.4, Chattanooga, TN, October, 2010.

Hyams, Daniel G., Kress, Reid, and Swafford, Tim W., “CFD‐Driven Agent‐Based Dispersion Modeling of the Y‐12 National Security Complex,” UTCCECSSimCenter201001R, September 2010.

Ji, L., Sreenivas, K., Hyams, D., and Wilson, R., “A Parallel Universal Mesh Deformation Scheme for Hydrodynamic Applications,” Proceedings of the 28th ONR Symposium on Naval Hydrodynamics, Pasadena, CA, 1217 Sep. 2010.

Betro, V. C., “Fully Anisotropic SplitTree Adaptive Refinement Mesh Generation Using Tetrahedral Mesh Stitching,” PhD Dissertation, University of Tennessee at Chattanooga, August 2010.

Hyams, D. G., Webster, R. W., and Sreenivas, K., “A Generalized Interpolative Interface for Parallel Unstructured Flow Solvers,” 40th Fluid Dynamics Conference and Exhibit, Chicago, Illinois, June 281, 2010. Paper No. 20105097.

Hyams, D. G., Webster, R. W., and Sreenivas, K., “A Generalized Axisymmetric Boundary Condition Method for Parallel Unstructured Field Solvers,” Proceedings of ASME Gas Turbine Technical Congress and Exposition 2010, Glasgow, UK, June 1418, 2010. Paper GT201023414.

Ji, L., Wilson, R., Sreenivas, K., and Hyams, D., “A Parallel Universal Mesh Deformation Scheme,” 28th AIAA Applied Aerodynamics Conference, June 2010, Chicago, AIAA20104938.

Kapadia S., Anderson W.K., and Workman N., “Computational Design of Tubular Solid Oxide Fuel Cells,” ASME 2010 8th International Fuel Cell Science, Engineering & Technology Conference, June 1416, 2010, Brooklyn, New York.

Wang, Li, Mavriplis, Dimitri J. and Anderson, W. Kyle, “Unsteady Discrete Adjoint Formulation for Highorder Discontinuous Galerkin Discretizations in Timedependent Flow Problems,” 48th AIAA Aerospace Science Meeting, January 2010, Orlando, FL, AIAA2010367.

Johnson, B. C., Webster, R. S., and Sreenivas K. “A Numerical Investigation of SDuct Flows with BoundaryLayer Ingestion,” 48th AIAA Aerospace Science Meeting, January 4thJanuary 7th, 2010, Orlando, Florida, AIAA2010841.

Webster, R., Hyams, D., Sreenivas, K., “Unstructured Grid Technology Applied to Axialflow Compressors,” AIAA20101605, 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, Orlando, Florida, Jan. 47, 2010.
2009 (back to top)

Li Wang and Dimitri J. Mavriplis, “Adjointbased hp Adaptive Discontinuous Galerkin Methods for the 2D Compressible Euler Equations,” Journal of Computational Physics, Vol. 228, Issue 20, pp 76437661, November 2009.

Daniel G. Hyams and David L. Whitﬁeld, “Atmospheric Dispersion at Spatial Resolutions Below Mesoscale for University of Tennessee SimCenter at Chattanooga: Final Report,” DOE Award DEFG0205ER64076, September 2009.

Karman, Jr., S.L., Mitchell, B., Sawyer, S., and Whitt, J., “Numerical Solutions for the CAWAPI Configuration on Unstructured Grids at UTSimCenter, United States,” in Understanding and Modeling Vortical Flows to Improve the Technology Readiness Level for Military Aircraft, NATO RTOTRAVT113, pp.14136, RTO/NATO, 2009.

Sivakumar, P., Hyams, D.G., Taylor, L.K., and Briley, W.R., “A PrimitiveVariable Riemann Method for Solution of the ShallowWater Equations with Wetting and Drying,” Journal of Computational Physics, Vol. 228, No.19, pp. 74527472, 2009.

Arabshahi, A., Webster, R., Sreenivas, K., Hyams, D.G., and Whitfield, D.L., “Numerical Simulation of Reacting and NonReacting Nozzle Flows,” AIAA20094858, 45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Denver Colorado, August 2009.

Sreenivas, K., Taylor, Lafayette K., Briley, W. Roger, “Unsteady Flow Simulations for an AerotonomyDesigned SyntheticJet Airfoil,” UTCCECSSimCenter200902R, June 2009.

Kapadia, S., Anderson, W. K., and Burdyshaw, C., “Channel Shape Design of Solid Oxide Fuel Cells,” UTCCECSSimCenter200901, June 2009.

Karman, S., et al., "CFD Modeling of F35 Using Hybrid Unstructured Meshes," AIAA Paper 20093662, 19th AIAA CFD Conference, San Antonio, TX, June 2225 2009

Dweik, Z., Briley, W.R., Swafford, T.W., and Hunt, B., “Computational Study of the Heat Transfer of the BuoyancyDriven Rotating Cavity with Axial Throughflow of Cooling Air,” GT200959978, ASME Turbo EXPO 2009, June 812, 2009, Orlando, FL.

Dweik, Z., Briley, W.R., Swafford, T.W., and Hunt, B., “Computational Study of the Unsteady Flow Structure of the BuoyancyDriven Rotating Cavity with Axial Throughflow of Cooling Air,” GT200959969, ASME Turbo EXPO 2009, June 812, 2009, Orlando, FL.

Anderson, W.K., Karman, S.L., and Burdyshaw, C., “Geometry Parameterization Method for Multidisciplinary Applications,” AIAA Journal, Vol. 47, No. 6, June 2009.

Chen, JP, Johnson, B., Hathaway, M.D., and Webster, R.S., “Flow Characteristics of Tip Injection on Compressor Rotating Spike via TimeAccurate Simulation,” Journal of Propulsion and Power, Vol. 25, No. 3, MayJune, 2009, pp. 678687.

Boelens, O.J., Badcock, K.J., Görtz, S., Morton, S., Fritz, W., Karman, Jr., S.L., Michal, T., and Lamar, J.E., “F16XL Geometry and Computational Grids Used in Cranked Arrow Wing Aerodynamics Project International,”Journal of Aircraft, Vol. 46, No. 2, March–April 2009, pp. 369376.

Kapadia, S. and Anderson, W.K., “Sensitivity Analysis for Solid Oxide Fuel cells using a ThreeDimensional Numerical Model,” Journal of Power Sources, Volume 189, Issue 2, April, 2009, Pages 10741082

Kapadia, S., Anderson, W. K., Elliott, L., and Burdyshaw, C., “Adjoint based Sensitivity Analysis and Error Correction Methods applied to Solid Oxide Fuel Cells,” ASME Journal of Fuel Cell Science and Technology, Vol. 6, No. 2, 2009.

Elliott, L., Anderson, W. K., and Kapadia, S., “Solid Oxide Fuel Cell Design and Optimization with Numerical Adjoint Techniques,” ASME Journal of Fuel Cell Science and Technology, Vol. 6, No. 4, 2009.

Karman, Jr., S.L., and Sahasrabudhe, M., “Unstructured Elliptic Smoothing Revisited,” 47th Aerospace Sciences Meeting and Exhibit, January 5th  January 9th, 2009, Orlando, Florida, AIAA20091362.

Wang, Li and Mavriplis, Dimitri J., “Adjointbased hp Adaptive Discontinuous Galerkin Methods for the Compressible Euler Equations,” 47th AIAA Aerospace Science Meeting, January 2009, Orlando, FL, AIAA20090952.
2008 (back to top)

Sivakumar, P., Hyams, D.G., Taylor, L.K., and Briley, W.R., “PrimitiveVariable Riemann Fluxes for Solution of the Shallow Water Equations with Embedded Wet/Dry Interfaces,” UTCCECSSimCenter200806, November 2008.

Wilson, R., Lei, J., Karman, Jr., S.L., Hyams, D., Sreenivas, K., Taylor, L., and Whitfield D., 2008, “Simulation of Large Amplitude Ship Motions for Prediction of FluidStructure Interaction,” Proceedings of the 27th ONR Symposium on Naval Hydrodynamics, Seoul, Korea, 510 Oct. 2008.

Karman, Jr., S.L., and Wilson, R., 2008, “Hierarchical Unstructured Mesh Generation with General Cutting for Free Surface Simulations,” Proceedings of the 27th ONR Symposium on Naval Hydrodynamics, Seoul, Korea, 510 Oct. 2008.

Lee, D., Maki, K., Wilson, R., Troesch, A., and Vlahopoulos, N., “Dynamic Response of a Marine Vessel Due to WaveInduced Slamming,” Int. Sym. On VibroImpact Dynamics of Ocean Systems and Related Problems, Troy, Michigan, 23 Oct. 2008.

Lange, K. and Anderson, W.K. “Using Sensitivity Derivatives for Design and Computing Error Bounds in an Atmospheric Plasma Discharge Simulation.” 61st Annual Gaseous Electronics Conference, October 2008.

Briley, W. Roger and McDonald, H., “Reflections on the Evolution of Implicit NavierStokes Algorithms,” UTCCECSSimCenter200804, September 2008.

Wilson, Robert V., “A Review of Computational Ship Hydrodynamics,” UTCCECSSimCenter200803, September 2008.

Anderson, W. Kyle, Karman, Jr., S.L., and Burdyshaw, Chad, “Geometry Parameterization Using Control Grids,” AIAA 2008Presented at the 12th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, Victoria, BC, September 1012, 2008.

Lange, K. and Anderson, W.K. “Sensitivity Derivatives for Plasma Discharge Simulations.” AIAA20085930. 12th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, September 2008.

Sahasrabudhe, M., “Unstructured Mesh Generation and Manipulation based on Elliptic smoothing and Optimization,” Ph.D. Dissertation, University of Tennessee at Chattanooga, August 2008.

Kapadia, S., Anderson, W. K., and Elliott, L., “Sensitivity Analysis of ThreeDimensional Solid Oxide Fuel Cell Model,” 6th International ASME Conference on Fuel Cell Science, Engineering, and Technology, Denver, June 1618, 2008.

Whitfield, D.L, Pankajakshan, R., Sreenivas, K., and, Taylor, L.K. “Numerical Derivatives, MatrixVector Product, and Richardson Extrapolation Using Complex Variables,” UTCCECSSimCenter200801, March 2008.

Hajjawi, M., Taylor, L., and Nichols, III, D.S., “Assessment and Modification for Reynolds Stress Transport Turbulence Model Flow Prediction,” AIAA20080568, 46th AIAA Aerospace Sciences Meeting and Exhibit, January 2008.

Hajjawi, M., Taylor, L., and Nichols, III, D.S., “Assessment of Filtered Based RANS Turbulence Model for Unsteady Separated Flow Prediction,” AIAA20080670, 46th AIAA Aerospace Sciences Meeting and Exhibit, January 2008.

Karman, Jr., S.L. and Betro, V., “Parallel Hierarchical Unstructured Mesh Generation with General Cutting,” AIAA20080918, Reno, NV, Jan. 2008.
2007 (back to top)

Burdyshaw, C.E. and Anderson, W.K., “Advances in Discrete Sensitivity Methods Applied to Uncertainty Analysis NATO Research and Technology Organisation,” RTOMPAVT147, Conference on Computational Uncertainty in Military Vehicle Design, Papers presented at the RTO Applied Vehicle Technology Panel (AVT) Symposium held in Athens, Greece on 36 December 2007.

Olivieri, A., Pistani, F., Wilson, R., Campana, E., and Stern, F., “Scars and Vortices Induced by Bow and Shoulder Wave Breaking,” Vol. 129, J. Fluids Eng., Nov. 2007, pp. 14451459.

Pankajakshan, Ramesh, Sreenivas, Kidambi, Mitchell, Brent, and Whitfield, David L., “CFD Simulations of Class 8 Trucks,” 2007014293, SAE 2007 Commercial Vehicle Engineering Congress & Exhibition, October 2007.

Pankajakshan, R., Mitchell, B. and Whitfield, D., “FullScale Simulations of Drag Reduction Devices for Class 8 Trucks,” In The Aerodynamics of Heavy Vehicles II: Trucks, Buses, and Trains. Lecture Notes in Applied and Computational Mechanics. Springer Berlin/Heidelberg, pp. 339348. 2009.

Sreenivas, K., Mitchell, B., Nichols, III, D.S., Hyams, D.G., and Whitfield, D.L., “Computational Simulation of the GCM TractorTrailer Configuration,” Aerodynamics of Heavy Vehicles II: Trucks, Buses, and Trains, Lake Tahoe, August 2007.

Wilson, R., Nichols, III, S., Mitchell, B., Karman, S., Betro, V., Hyams, D., Sreenivas, K., Taylor, L., Briley, R., and Whitfield D., “Simulation of a Surface Combatant with Dynamic Ship Maneuvers,” 9th Int. Conf. in Num. Ship Hydro., University of Michigan, 58 Aug. 2007.

Kapadia, S., Anderson, W.K., Elliott, L, and Burdyshaw, C., “Adjoint method for solidoxide fuel cell simulations,”Journal of Power Sources, Vol. 166, 2007, pp. 376385.

Arabshahi, A. and Whitfield, D. L., “Computational of Dynamic Stability and Control Derivatives,” THEC Final Report, January 2005 – July 2007.

Arabshahi, A., Webster, R. S., Briley, W. R., and Whitfield, D. L., “Advancement and Verification of the NavierStokes Flow Solver for Rocket Motor Internal Flows,” THEC Final Report, July 2005 – June 2007.

Kapadia, S., Anderson, W. K., and Elliott, L., “Design and Sensitivity Analysis of Solid Oxide Fuel Cells Using Discrete Adjoint Method,” 5th International Energy Conversion Engineering Conference and Exhibit (IECEC), 25  27 June 2007, St. Louis, Missouri, AIAA 20074832.

Kapadia, S., Anderson, W. K., and Elliott, L., and Burdyshaw, C., “Adjoint Based Sensitivity Analysis And Error Correction Methods Applied To Solid Oxide Fuel Cells,” Presented at ASME 5th International Fuel Cell Science, Engineering & Technology Conference, June 18  20, 2007, New York, FuelCell200725157.

Wilson R., Carrica, P., and Stern F., “Simulation of Ship Breaking Bow Waves and Induced Vortices and Scars,” Vol. 54, No. 4 Int. J. Num. Methods Fluids, June 2007, pp. 419451.

Carrica, P., Wilson R., and Stern F., “An Unsteady SinglePhase Level Set Method for Viscous Free Surface Flows,” Vol. 53, No. 2, Int. J. of Num. Methods Fluids , Jan. 2007, pp. 229256.

Arabshahi, A., Sreenivas, K., Nichols, III, D.S., Mitchell, B., Taylor, L., and Whitfield, D., “Computational Analysis of Turbulent Internal Flow in Ballistic Rocket Motors,” AIAA20071449, 45th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, Jan. 811, 2007.

Karman, Jr., S.L. and Sahasrabudhe, M., “Unstructured Adapted Elliptic Smoothing,” AIAA20070559, 45th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, Jan. 811, 2007.

Karman, Jr., S.L., Mitchell, B., Sawyer, S., and Whitt, J., “Unstructured Grid Solutions of CAWAPI F16XL by UT SimCenter,” AIAA20070681, 45th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, Jan. 811, 2007.

Sreenivas, K., Nichols, III, D.S., Hyams, Mitchell, B., Sawyer, S., and Whitfield, D.L., “Computational Simulation of Heavy Trucks,” AIAA20071087, 45th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, Jan. 811, 2007.

Sreenivas, K., Mitchell, B., Sawyer, S., Karman, Jr., S.L., Nichols, III, D.S., and Hyams, D., “Computational Prediction of Forces and Moments for Transport Aircraft,” AIAA20071088, 45th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, Jan. 811, 2007.

Pankajakshan, R., Mitchell, B.J., and Taylor, L.K., “Simulation of Unsteady TwoPhase Flows using a Parallel EulerianLagrangian Approach,” AIAA20070340, 45th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, Jan. 811, 2007.

Nichols, III, D.S., Sreenivas, K., Karman, Jr., S.L., and Mitchell, B., “Turbulence Modeling for Highly Separated Flows,” AIAA20071407, 45th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, Jan. 811, 2007.

Karman, Jr., S.L., “Unstructured Viscous Layer Insertion Using LinearElastic Smoothing,” AIAA Journal, Volume 45, Number 1, pp. 168180, January 2007.
2006 (back to top)

Tahara, Y., Wilson, R., Carrica, P., and Stern, F., “RANS Simulation of a Container Ship Using a SinglePhase Level Set Method with Overset Grids and the Prognosis for Extension to SelfPropulsion Simulator,” Vol. 11, No. 4, J. Marine Science and Technology, 2006, pp. 209228.

Almeida, T.G., Walker, D.T., Leighton, R.I., Alajbegovic, A., Pankajakshan, R., Taylor, L.K., Whitfield, D.L., and Ceccio, S.L., “A ReynoldsAveraged Model for the Prediction of Friction Drag Reduction by Polymer Additives,” 26th Symposium on Naval Hydrodynamics, Rome Italy, September. 1722, 2006.

Carrica, P.M., Wilson, R.V., Noack, R., Xing, T., Kandasamy, M., Shao, J., Sakamoto, N., and Stern, F., “A Dynamic Overset, SinglePhase Level Set Approach for Viscous Ship Flows and Large Amplitude Motions and Maneuvering,” 26th Symposium on Naval Hydrodynamics, Rome Italy, September. 1722, 2006.

Wilson, R.V., Nichols, III, D.S., Mitchell, B., Karman, S.L., Hyams, D.G., Sreenivas, K., Taylor, L.K., Briley, W.R., and Whitfield, D.L., “Application of an Unstructured Free Surface Flow Solver for High Speed Transom Stern Ships,” 26th Symposium on Naval Hydrodynamics, Rome Italy, September. 1722, 2006.

Arabshahi, A., Webster, R.S., Briley, W.R., and Whitfield, D. L., “Numerical Analysis of Solid Propellant Rocket Motor Internal Flows,” AIAA20065114, July, 2006.

Sreenivas, K., Taylor, L., and Briley, W.R.,“A Global Preconditioner for Viscous Flow Simulations at All Mach Numbers,” AIAA20063852, June 2006.

Karman, Jr., S.L., Anderson, W.K., Sahasrabudhe, M., “Mesh Generation Using Unstructured Computational Meshes and Elliptic Partial Differential Equation Smoothing,” AIAA Journal, Volume 44, Number 6, pp. 12771286, June 2006.

Hyams, D., Sreenivas, K., and Whitfield, D.L., “Parallel FAS Multigrid for Arbitrary Mach Number, High Reynolds Number Unstructured Flow Solvers,” AIAA20062821, June 2006

Nichols, III, D.S., Mitchell, B., Sreenivas, K., Taylor, L., Whitfield, D.L., and Briley, W.R., “Aerosol Propagation in an Urban Environment,” AIAA 20063726, June 2006.

Burdyshaw, C.E., “Achieving Automatic Concurrency Between Computational Field Solvers and Adjoint Sensitivity Codes,” Ph.D. Dissertation, University of Tennessee at Chattanooga, May 2006.

Wilson, R., Carrica, P., and Stern, F., “Unsteady RANS Method for Ship Motions with Application to Roll for a Surface Combatant,” Computers & Fluids, Vol. 35, p.501524, 2006.

Carrica, P., Wilson R., and Stern F., “Unsteady RANS Simulation for Forward Speed Diffraction of a Surface Combatant,” Computers & Fluids, Vol. 35, p.545570, 2006.

Wilson, R., Carrica, P., and Stern F., “URANS Simulation for a HighSpeed Transom Stern Ship with Breaking Waves,” Int. J. of CFD, Vol. 20, No. 2, Feb. 2006, pp.105125.

Stern, F., Wilson, R., and Shao, J., 2006, “Quantitative V&V of CFD simulations and certification of CFD codes,”Int. J. for Num. Methods in Fluids, Volume 50, Issue 11 , Pages 1335  1355.

Sahasrabudhe, M., Karman, Jr., S.L., and Anderson, W.K., “Grid Control of Viscous Unstructured Meshes Using Optimization,” AIAA2006532, 44th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, Jan. 912, 2006.

Ellis, D., Karman, Jr., S.L., and Novobilski, A., Haimes, R., “3D Visualization and Manipulation of Geometry and Surface Meshes,” AIAA2006944, 44th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, Jan. 912, 2006.

Nichols, III, D.S., Hyams, D., Sreenivas, K., Mitchell, B., Taylor, L., and Whitfield, D., “An Unstructured Incompressible MultiPhase Solution Algorithm,” AIAA20061290, 44th AIAA Aerospace Sciences Meeting and Exhibit, January 2006.

Sreenivas, K., Pankajakshan, R., Nichols, III, D.S., Mitchell, B., Taylor, L., and Whitfield, D.L., “Aerodynamic Simulation of Heavy Trucks with Rotating Wheels,” AIAA20061394, 44th AIAA Aerospace Sciences Meeting and Exhibit, January 2006.

Chen, J.P., Webster, R.S., Hathaway, M.D., Herrick, G.P., and Skoch, G.J., “Numerical Simulation of Stall and Stall Control in Axial and Radial Compressors,” AIAA20060418, January 2006.
2005 (back to top)

McDonald, Henry, “Observations on the Columbia Accident,” Organization at the Limit, Lessons from the Columbia Disaster, Edited by W. H. Starbuck and M. Farjoun, Blackwell Publishing, pp. 336346, 2005.

McCallen, R., Salari, K., Ortega, J., Castellucci, P., Paschkewitz, J., Eastwood, C., Dechant, L., Hassan, B., Pointer, W. D., Browand, F., Leonard, A., Rubel, M., Ross, J., Heineck, J.T., Walker, S., Storms, B., Roy, C., Whitfield, D.L., Pankajakshan, R., Taylor, L., Sreenivas, K., and Englar, R., “DOE’s Effort to Reduce Truck Aerodynamic Drag through Joint Experiments and Computations Leading to Intelligent Design,” SAE International, 2005.

Sakamoto, N., Wilson, R., and Stern, F., “RANS Simulations for High Speed Ships in Deep and Shallow Water,”Proceedings of FAST 2005, 8th Int. Conf. on Fast Sea Transportation, June 2730, 2005, SaintPetersburg, Russia.

Wilson, R. and Stern, F., “URANS Simulations For A HighSpeed Transom Stern Ship With Breaking Waves,”Proceedings of FAST 2005, 8th Int. Conf. on Fast Sea Transportation, June 2730, 2005, SaintPetersburg, Russia.

Weymouth, G. Wilson, R., and Stern, F., “RANS CFD Prediction of Pitch and Heave Ship Motions in Head Seas,”Journal Ship Research, Vol. 49(2), June, 2005, pp. 8097.

Tahara, Y., Wilson, R., and Carrica, P., “Comparison of Free Surface Capturing and Tracking Approaches in Application to Modern Container Ship and Prognosis for Extension to SelfPropulsion Simulator,” Proceedings of the CFD Workshop Tokyo 2005, Tokyo, Japan, 911, March 2005.

Miller, R. Wilson, R., Carrica, P., and Gorski, J., “RANS Simulation of a Naval Surface Combatant Using a SinglePhase Level Set Method with Overset Grids,” Proceedings of the CFD Workshop Tokyo 2005, Tokyo, Japan, 911, March 2005.

Carrica, P., Wilson, R., and Stern, F., “Unsteady RANS Simulation for Forward Speed Diffraction of a Surface Combatant,” Proceedings of CFD Tokyo 2005 Workshop, Tokyo Japan, March 2005.

Wilson, R., Carrica, P., and Stern, F., “RANS Simulation for a Container Ship using a Single Phase Level Set and Overset Grid Method,” Proceedings of CFD Tokyo 2005 Workshop, Tokyo Japan, March 2005.

Kandasamy, M., Xing, T., Wilson, R., and Stern, F., “Vortical and Turbulent Structures and Instabilities in Unsteady FreeSurface Wave Induced Separation,” Proceedings of 5th Osaka Colloquium, March 1415, 2005, Osaka Japan.

Taylor, L.K., Pankajakshan, R., Briley, W.R., and Whitfield, D. L., “Scalable Parallel Implicit Algorithm for Advanced Turbulence Closures,” AIAA Paper No. 20050876, 43rd Aerospace Sciences Meeting and Exhibit, Reno, NV, January 2005.

Sreenivas, K., Hyams, D.G., Nichols, III, D. S., Mitchell, B., Taylor, L.K., Briley, W.R., and Whitfield, D.L., “Development of an Unstructured Parallel Flow Solver for Arbitrary Mach Numbers,” AIAA Paper No. 20050325, 43rd Aerospace Sciences Meeting and Exhibit, Reno, NV, January 2005.

Burdyshaw, C.E. and Anderson, W.K., “A General and Extensible Unstructured Mesh Adjoint Method,” AIAA Paper No. 20050335, 43rd Aerospace Sciences Meeting and Exhibit, Reno, NV, January 2005.
2004 (back to top)

Arabshahi, A. and Janus, J.M., “A Multiblock Compressible NavierStokes Flow Solver Applied to Complex Launch Vehicles,” AIAA Journal of Spacecraft and Rockets, Vol. 41, No. 3, pp. 469472, MayJune 2004.

Karman, Jr., S.L., “Hierarchical Unstructured Mesh Generation,” AIAA Paper No. 20040613, 42nd Aerospace Sciences Meeting and Exhibit, Reno, NV, January 2004.

Lambert, B. K., “Development and Validation of a Time Accurate Algorithm for Low Mach Number Compressible Flow,” PhD Dissertation, University of Tennessee at Chattanooga, December 2004.

Wilson, R., Shao, J., and Stern, F., “Discussion: “Criticisms of the “Correction Factor” Verification Method” (Roache, P., 2003, ASME J. Fluids Eng., 125, pp. 732733),” ASME J. Fluids Eng, Vol. 126, No. 4, 2004.

Wilson, R., Carrica, P., Hyman, M., and Stern, F., “A Steady and Unsteady LevelSet Method for Large Amplitude Ship Motions and Maneuvering,” Proceedings 25th ONR Symposium on Naval Hydrodynamics, St. Johns, Canada, August 2004.

Stern, F., Wilson, R., and Shao, J., “Quantitative Approach to V&V of CFD Simulations and Certification of CFD Codes with Examples,” Proceedings International Symposium Advances Computational Heat Transfer (Invited paper), KirkenesBergen, Norway, 1924 April 2004.

Xing, T., Kandasamy, M., Wilson, R. and Stern, F., “DES and RANS of Unsteady Freesurface Flows,” 42nd AIAA Aerospace Sciences Meeting, Reno, Nevada, 58 Jan 2004, Division for Fluid Dynamics.
2003 (back to top)

Briley, W.R., Pankajakshan, R., Taylor, L.K., Gorski, J.J., Slomski, J.F., Dommermuth, D.G., Rottman, J.W., and Innis, G.E., “Submerged Wakes in Littoral Regions,” 2003 DoD HPCMP Users Group Conference, Bellevue, WA, June, 2003.

Briley, W.R., Taylor, L.K., and Whitfield, D.L., “HighResolution Viscous Flow Simulations at Arbitrary Mach Number,” Journal of Computational Physics, 184(1):79105, 2003.

Lambert, B.K., Taylor, L.K., and Briley, W.R., “Evaluation of a Preconditioned Flow Solver for a Broad Range of Mach Number and Temperature Ratio,” In Numerical Simulations of Incompressible Flows, edited by M.M. Hafez, University of California, Davis, pp. 605621.

Sreenivas, K., Cash, A.N., Hyams, D.G., and Taylor, L.K., “Computational Study of PropulsorHull Interactions,” AIAA Paper No. 20031262, 41st Aerospace Sciences Meeting and Exhibit, Reno, NV, January 2003.

Blades, E., Sreenivas, K., and Hyams, D.G., “Arbitrary Overlapping Interfaces for Unsteady Unstructured Parallel Flow Simulations,” AIAA Paper No. 20030276, 41st Aerospace Sciences Meeting and Exhibit, Reno, NV, January 2003.

Pankajakshan, R., Taylor, L.K., Briley, W. R., and Whitfield, D.L., “Arbitrary Mach Number Flow Simulations,” AIAA Paper No. 20031236, 41st Aerospace Sciences Meeting and Exhibit, Reno, NV, January 2003.

Hindi, M.M., White, C.A., and Kozub, R.L., “Double Kshell ionization probability in Mn54,” Physical Review C 68, 014306 (2003), July 25, 2003.

Weymouth, G., Wilson, R., and Stern, F., “RANS CFD Prediction of Pitch and Heave Ship Motions in Head Seas,” Proceedings of the 8th Int. Conf. on Numerical Ship Hydrodynamics, Busan, S. Korea, September 2003.

Stern F., Wilson, R., Longo, J., Carrica, P., Xing, T., Tahara, Y., Simenson, C., Kim, J., Shao, J., Irvine, M., Kandysamy, M., Ghosh, S., and Weymouth, G., “Paradigm for Development of Simulation Based Design for Ship Hydrodynamics,” Proceedings of the 8th Int. Conf. on Numerical Ship Hydrodynamics, Busan, S. Korea, September 2003.

Stern, F., Wilson, R., and Shao, J., “Statistical Approach to CFD Code Certification,” AIAA 20036345, Applied Aerodynamics Special Session on CFD Uncertainty, 41st Aerospace Sciences Meeting, Reno, Nevada, 69 January 2003.
2002 (back to top)

Lucien, V., AlpucheAviles, M. A., GravesBrook, M. K., and Wipf, D. O., “Electrochemical study and surface analysis of passive films on AISI 316 stainless steel grown in alkaline solutions,” 15th International Corrosion Congress, September 2227, 2002.

Nichols, III, D.S., “Development of a Free Surface Method Utilizing an Incompressible MultiPhase Algorithm to Study the Flow About Surface Ships and Underwater Vehicles,” PhD Dissertation, Mississippi State University, August 2002.

Arabshahi, A. and Gibeling, H. J., “Computational Hydrodynamics for an Autonomous Underwater Vehicle with Moving Control Surfaces,” FEDSM200231428, ASME 2002 Fluids Engineering Division Summer Meeting, Montreal, Canada, July 2002.

Arabshahi, A., Tangirala, S., Dzielski, J.E., and Gibeling, H.J., “CFD Based Prediction of Stability and Control Derivatives for Autonomous Underwater Vehicles,” the 8th International Conference on Numerical Grid Generation in Computational Field Simulations, Honolulu, Hawaii, June 2002.

Arabshahi, A., Boger, D. A., Lindau, J. L., Zajaczkowski, F. J. , “CFD Validation and Development for CCAT Design Analysis,” the CCAT board, ONR PMS 415, Applied Research Laboratory, State College, PA, February 2002.

Burg, C. O. E., Sreenivas, K., Hyams, D. G., and Mitchell, B., “Unstructured Nonlinear Free Surface Flow Solutions: Validation and Verification,” AIAA Paper No. 20022977, 32nd AIAA Fluid Dynamics Conference and Exhibit, St. Louis, MO, June 2002.

Sreenivas, K., Hyams, D., Mitchell, B., Taylor, L.K., Marcum, D., and Whitfield, D.L., “Computation of Vortex Intensive Incompressible Flow Fields,” AIAA Paper No. 20023306, 32nd AIAA Fluid Dynamics Conference and Exhibit, St. Louis, MO, June 2002.

Blades, E.L., Marcum, D., and Mitchell, B., “Simulation of Spinning Missile Flow Fields Using U2NCLE,” AIAA Paper No. 20022797, 32nd AIAA Fluid Dynamics Conference and Exhibit, St. Louis, MO, June 2002.

Eglin, J.L., Dequeant, M.Q., GravesBrook, M.K., and Smith, L.T., “Hydrolysis of Cyanophenols at Bimetallic Re2(III,III) Core,” Abstracts of Papers, 223rd ACS National Meeting, April 711, 2002.

Blades, E.L., Marcum, D.L., and Mitchell, B., “Euler and NavierStokes Simulation of the Aerodynamics of a Spinning Missile with Dithering Control Surfaces.” MSSUCOEERC0202, Mississippi State University, Feb. 2002.

Pankajakshan, R., Taylor, L.K., Sheng, C., Briley, W.R., and Whitfield, D.L., “Scalable Parallel Implicit Multigrid Solution of Unsteady Incompressible Flows,” Frontiers of Computational Fluid Dynamics 2002, edited by D. A. Caughey and M. M. Hafez, World Scientific Publishing Company PTE. LTD., Singapore, pp. 181195, 2002.

Briley, W.R, Keynote Address: Computational Fluid Dynamics and Computational Engineering Education. Forum on Advances in Fluids Engineering Education, FEDSM200231378, ASME Joint U.S.European Fluids Engineering Division Summer Meeting, Montreal, Canada, July 2002.

Pankajakshan, R., Remotigue, M.G., Taylor, L.K., Jiang, M., Briley, W.R., and Whitfield, D.L., “Validation of ControlSurface Induced Submarine Maneuvering Simulations Using UNCLE,” 24th Symposium on Naval Hydrodynamics, Fukuoka, Japan, July 813, 2002.

Chen, J.P., and Briley, W.R, “Development of a Parallel Turbomachinery Flow Solver,” MSSUCOEERC02109 (NASA Grant NAG32176), June 2002.

Sreenivas, K., Hyams, D.G., Sheng, C., Jayaraman, B., Wang, X., Mitchell, B., Jiang, M.Y., Pankajakshan, R., Taylor, L.K., Gaither, K.P., Gaither, A., Beeland, H., Marcum, D.L., Briley, W.R., and D. L. Whitfield, “PhysicsBased Maneuvering Simulations for Tiltrotor Aircraft,” MSU Report No. MSSUCOEERC0206 (NASAARC Grant NAG21232), April 2002.

Sreenivas, K., Hyams, D.G., Burg, C.O.E., Mitchell, B.J., Sheng, C., Jayaraman, B., Pankajakshan, R., Brewer, W.H., Nichols III, D.S., Taylor, L.K., Remotigue, M.G., Wang, X., Jiang, M.Y., Gaither, K.P., Gaither, A., Beeland, H.L., Newman, III, J.C., Marcum, D.L., Briley, W.R., and Whitfield, D.L., “Computational Engineering Research Supporting the Analysis and Design of Marine and Aerospace Vehicles,” MSU Report No. MSSUCOEERC0209 (ONR Grant N000149910751), May 2002.

Burg, C.O.E., Sreenivas, K., and Hyams, D.G., “Unstructured Nonlinear Free Surface Simulations for the FullyAppended DTMB Model 5415 Series Hull Including Rotating Propulsors,” 24th Symposium on Naval Hydrodynamics, Fukaoka, Japan, July 2002.

Newman, III, J.C., Pankajakshan, R., Whitfield, D.L., and Taylor, L.K., “Computational Design Using RANS,” 24th Symposium on Naval Hydrodynamics, Fukuoka, Japan, July 813, 2002.

Remotigue, M.G., Pankajakshan, R., Jiang, M., Taylor, L.K., Briley, W.R., and Whitfield, D.L., “Dynamic Grid Generation for Simulation of Submarine Maneuvers: Part II,” 8th International Conference on Numerical Grid Generation in Computational Field Simulations, Honolulu, Hawaii, June, 2002.

Brook, R.G., Oppenheimer, P.E., Weatherford, C.A., Banicescu, I., and Zhu, J., “Accuracy studies of a parallel algorithm for solving the hydrodynamic formulation of the timedependent Schrodinger equation,” Journal of Molecular Structure (Theochem), Vol. 592, pp. 6977, 2002.

Nielsen, E.J., and Anderson, W.K., “Recent Improvements in Aerodynamic Design Optimization on Unstructured Meshes,” AIAA Journal, Vol. 40, No. 6, June 2002, pp. 11551163.

Rumsey, C.L., Gatski, T.B., Anderson, W.K., and Nielsen, E.J., “Isolating Curvature Effects in Computing WallBounded Turbulent Rows,” Intl. J. Heat and Fluid Flow, Vol. 22, 2002, pp. 573582.

Stern F., and Wilson, R., “Author’s Closure,” ASME J. Fluids Eng., Vol. 124(3), 2002, pp.810811.

Wilson R. and Stern F., “Unsteady RANS Simulation of a Surface Combatant with Roll Motion,” Proceedings of 24th Symposium on Naval Hydrodynamics, Fukuoka, Japan, July 813, 2002.

Wilson R. and Stern F., “Verification and Validation for RANS Simulation of a Naval Surface Combatant,” 40th Aerospace Sciences Meeting and Exhibit, Reno, Nevada, AIAA 20020904, Jan. 2002.
2001 (back to top)

Grayson, B. A., Wolan, J. T., GravesBrook, M. K., Bledsoe, M., Kirchner, K., Saddow, S. E., "Comparison of 3CSiC films grown by CVD on Si(111) and Si(211) substrates," Materials Research Symposium Proceedings (2001), 604(Silicon Carbide: Materials, Processing and Devices).

Nelson, A. E., GravesBrook, M. K., Schulz, K. H., "Analysis of CeriumZirconium Mixed Metal Oxides by XRay Phtoelectron Spectroscopy," Surface Science Spectra (2001), 8(2), 126161.

Beggs, J. H., and Briley, W. R., "An Implicit Characteristic Based FDTD Method for Maxwell's Equations". Revision submitted to J. Applied Computational Electromagnetics Society, 2001.

Briley, W. R. and H. McDonald: An Overview and Generalization of Implicit NavierStokes Algorithms and Approximate Factorization. Journal of Computers and Fluids, Vol. 30, pp. 807828, 2001.

Marcum, D., Mitchell, B., Sreenivas, K., and Hyams, D., "Unstructured Grid Generation for LargeScale CFD Applications," ECCOMAS Computational Fluid Dynamics Conference 2001, University of Wales, Swansea, Wales, UK, September 2001 (Invited).

Pankajakshan, R., Taylor, L. K., Sheng, C., Briley, W. R., and D. L. Whitfield, "Scalable Parallel Implicit Multigrid Solution of Unsteady Incompressible Flows". Frontiers of Computational Fluid Dynamics 2000, Edited by D. A. Caughey and M. M. Hafez, World Scientific Publishing Company PTE. LTD., Singapore, 2001.

Stern F., Wilson R., Coleman H., and Paterson E., “Comprehensive Approach to Verification and Validation of CFD SimulationsPart 1: Methodology and Procedures,” ASME J. Fluids Eng., Vol. 123, Dec. 2001, pp. 793802.

Wilson R., Stern F., Coleman H., and Paterson E., “Comprehensive Approach to Verification and Validation of CFD SimulationsPart2: Application for RANS Simulation of A Cargo/Container Ship,” ASME J. Fluids Eng., Vol. 123, Dec. 2001, pp. 803810. Sivakumar, P., "Numerical Investigation of a Single Elliptic Impinging Jet", M.S. Thesis, Louisiana Tech University, November 2001.

Donatello, D., Sreenivas, K., and Taylor, L.K., “Computations of Unsteady Forces and Moments for SUBOFF Undergoing Prescribed Maneuvers Using U^{2}NCLE,” MSSUCOEERC0112, Mississippi State University. October 2001.

Lorenzo, L., Sreenivas, K., Mitchell, B., and Taylor, L.K., “Computation of Forces and Moments for the Airship AKRON and SUBOFF Using U^{2}NCLE,” MSSUCOEERC0111, Mississippi State University, October 2001.

Hyams, D.G., Sreenivas, K., Taylor, L.K., and Whitfield, D.L., “Incompressible Unstructured RANS Simulations for a Low Speed Centrifugal Compressor using U^{2}NCLE,” MSSUCOEERC0110, Mississippi State University, October 2001.

Newman, J.C., and Whitfield, D.L., "Sensitivity Derivative Analysis for Use in Computational Design," MSU Report MSSUCOEERC0106, Sept. 2001.

Brook, R. G., Oppenheimer, P. E., Weatherford, C. A., Banicescu, I., and J. Zhu, "Solving the Hydrodynamic Formulation of Quantum Mechanics: A Parallel MLS Method," International Journal of Quantum Chemistry, Vol. 85, pp. 263271, 2001.

Burdyshaw, Chad, "Quasi 3D MultiStage Turbomachinery PreOptimizer," M.S. Thesis, Mississippi State University, August 2001.

GravesBrook, Melissa, K., "Reactivity Studies of Dirhenium Octachloride (IV,IV) with Nitriles," M.S. Thesis, Department of Chemistry, Mississippi State University, August 2001.

Marcum, D., Mitchell, B., Sreenivas, K., and Hyams, D., "Unstructured Grid Generation for LargeScale CFD Applications," 1st MIT Conference on Computational Fluid and Solid Mechanics, Massachusetts Institute of Technology, Cambridge, MA, June 2001 (Invited)

Chen, J. P., and Briley, W. R., "A Parallel Flow Solver for Unsteady Multiple Blade Row Turbomachinery Simulations". ASME Paper 2001GT0348, presented at ASME TURBO EXPO 2001, New Orleans, LA, June 2001.

Webster, R.S., "A Numerical Study of the Conjugate ConductionConvection Heat Transfer Problem", Ph.D. Dissertation, Mississippi State University, May 2001.

Sreenivas, K, Hyams, D., Mitchell, B., Taylor, L., Briley, W. R., and Whitfield, D., “Physics Based Simulations of Reynolds Number Effects in Vortex Intensive Incompressible Flows,” NATO/RTO Symposium on Advanced Flow Management, Norway, May 2001.

Wilson R., Demuren A., and Carpenter M., “HigherOrder Compact Schemes for Numerical Simulation of Incompressible Flows, Part II: Applications”, Numerical Heat Transfer, Part B, 39(3), March 2001, pp. 231255.

Demuren A., Wilson R., and Carpenter M., “HigherOrder Compact Schemes for Numerical Simulation of Incompressible Flows, Part I: Theoretical Development”, Numerical Heat Transfer, Part B, 39(3), March 2001, pp. 207230.

Briley, W. R., Taylor, L. K., and Whitfield, D. L., "HighResolution Viscous Flow Simulations at Arbitrary Mach Number," Submitted to Journal of Computational Physics (also MSU Report No. MSSUCOEERC0104, March 2001).

Briley, W., Taylor, L., and Whitfield, D., "Scalable Flow Simulations with Rotating Components," Navigator, Naval Oceanographic Office: Major Shared Resource Center, Spring 2001, pp. 47.

Tao, Y. X., Xu, G., Mansoor, A. M., Kirmani, S. S., and W. R. Briley: Development of Ice Accretion Model Using Modular Approach. AIAA Paper 20010682, 39th Aerospace Sciences Meeting Conference and Exhibit, Reno, NV, January 2001.

Pankajakshan, R., Taylor, L. K., Sheng, C., Jiang, M. J., Briley, W. R., and D. L. Whitfield, "Parallel Efficiency in Implicit Multiblock, Multigrid Simulations, with Application to Submarine Maneuvering". AIAA Paper 20011093, 39th Aerospace Sciences Meeting Conference and Exhibit, Reno, NV, January 2001.

Nielsen, E. J., and Anderson, W. K., "Recent Improvements in Aerodynamic Design Optimization on Unstructured Meshes," AIAA 010596, Jan., 2001.

Anderson, W. K., Newman, J. C., Whitfield, D. L., and Nielsen, E. J., "Sensitivity Analysis for NavierStokes Equations on Unstructured Meshes using Complex Variables," AIAA Journal, Vol. 398, No. 1, pp.5663, January 2001.
2000 (back to top)

McDonald, H., Eaton, D., Ernst, R., Hopson, G., Kanki, B., Lahoff, J., Conahan, M., McKeown, J., Newman, J., Sackheim, R., Slenski, G., Strauss, R., Young, J., "Space Shuttle Independent Assessment Team (SIAT) Report," Report to Associate Administrator Office of Space Flight, National Aeronautics and Space Administration, 2000.

Chen, J., and Whitfield, D., "Computation of RotorStator Interaction Using the NavierStokes Equations (NASA Grant NAG31712, Final Report)," MSSUCOEERC0012, October 2000.

Gaither, J., Marcum, D., and Mitchell, B., "SolidMesh: A Solid Modeling Approach to Unstructured Grid Generation," 7th International Conference on Numerical Grid Generation in Computational Field Simulations, September 2000.

Beddhu, M., Pankajakshan, R., Jiang, M. Y., Taylor, L. K., Briley, W. R. and Whitfield, D. L., "Computation of Nonlinear Turbulent Free Surface Flows using the Parallel UNCLE code," 23rd Symposium on Naval Ship Hydrodynamics, Val de Reuil, France, September 1722, 2000.

Bourgoyne, D., Ceccio, S., Dowling, D., (University of Michigan, USA). Brewer, W., Jessup, S., Park, J., (Naval Surface Warfare Center, Carderock Division, USA). Pankajakshan, R., (Mississippi State University, USA)., "Hydrofoil Turbulent Boundary Layer Separation at High Reynolds Numbers," 23rd Symposium on Naval Ship Hydrodynamics, Val de Reuil, France, September 1722, 2000.

Beddhu, M., Pankajakshan, R., Jiang, M. Y., Taylor, L. K., Remotigue, M. G., Briley, W. R. and Whitfield, D. L., "Computation and Evaluation of CFD Results for Practical Ship Hull Forms," presented at Workshop on CFD in Ship Hydrodynamics, held in Gothenburg, Sweden, Sept. 1416, 2000.

Hyams, D.G., Sreenivas, K., Sheng, C., Nichols, S., Taylor, L.K., Briley, W.R., and Whitfield, D.L., "An Unstructured Multielement Solution Algorithm for Complex Geometry Hydrodynamic Simulations," 23rd Symposium on Naval Hydrodynamics, Val de Reuil, France, September 2000.

Jiang, M., Pankajakshan, R., Remotigue, M.G., and Taylor, L.K., "Dynamic Grid Generation for the Simulation of Submarine Maneuvers," Numerical Grid Generation in Computational Field Simulations. Proceedings of the 7th International Conference held at Whistler, British Columbia, and September 2000.

Sheng, C., Hyams, D., Sreenivas, K., Gaither, A., Marcum, D., and Whitfield, D., "ThreeDimensional Incompressible NavierStokes Flow Computations About Complete Configurations Using a Multiblock Unstructured Grid Approach," MSSUCOEERC0007, July, 2000.

Hyams, D.G , "An Investigation of Parallel Implicit Solution Algorithms for Incompressible Flows On Unstructured Topologies," Ph.D. Dissertation, Mississippi State University, May 2000.

Hyams, D.G., Sreenivas, K., Sheng, C., Briley, W.R., Marcum, D.L., and Whitfield, D.L., "An Investigation of Parallel Implicit Solution Algorithms for Incompressible Flows on Multielement Unstructured Topologies," Proc., 38th Aerospace Sciences Meeting & Exhibit, AIAA Paper No. 20000271, Reno, NV, January 2000.

Hyams, D.G., and Leylek, H. H., "A Detailed Study of Film Cooling Flow Physics: Part III  Streamwise Injection With Shaped Holes," Journal of Turbomachinery, Vol. 122, No. 1, January 2000.

Pankajakshan, R., Taylor, L.K., Jiang, M., Remotigue, M.G., Briley, W.R., and Whitfield, D.L., "Parallel Simulations for ControlSurface Induced Submarine Maneuvers," Proc., 38th Aerospace Sciences Meeting & Exhibit, AIAA Paper No. 20000962, Reno, NV, January 2000.

Arabshahi, A., Gibeling H. J., “Numerical Simulation of Viscous Flows about Underwater Vehicles,” OCEANS 2000 MTS/IEEE Conference & Exhibition, Providence, RI, September 2000.

Gaither, J., Marcum, D., and Mitchell, B., "SolidMesh: A Solid Modeling Approach to Unstructured Grid Generation," 7th International Conference on Numerical Grid Generation in Computational Field Simulations, September 2000.

Karman, Jr., S.L., Domel, N.D., “SPLITFLOW: Progress in 3 D CFD with Cartesian OmniTree Grids for Complex Geometries”, AIAA 20001006, 2000.

Alexandrov, N. M., Nielsen, E. J., Lewis, R. M., and Anderson, W K., "Model Management with VariableFidelity Physics Applied to Multielement Airfoil Optimization," AIAA 004886, Sept., 2000.

Wilson R., Paterson E., and Stern F., “Verification and Validation of a Naval Combatant,” Proceedings of CFD Gothenburg 2000 Workshop, Gothenburg Sweden, September 2000.
1999 (back to top)

Beddhu, M., Jiang, M.Y., Whitfield, D.L., and Taylor, L.K., "Computation of the Wetted Transom Stern Flow over Model 5415," Seventh International Conference on Numerical Ship Hydrodynamics, Nantes, France, July 1922, 1999.

Newman III, J.C., Anderson, W.K., and Whitfield, D.L., "A Step Size Independent Approach to Multidisciplinary Sensitivity Analysis and Design Optimization," Proc., 17th AIAA Applied Aerodynamics Conference, AIAA Paper No. 993101, June 1999.

Anderson, W.K., Whitfield, D.L., Newman III, J.C., Nielsen, E.J., "Sensitivity Analysis for the NavierStokes Equations on Unstructured Meshes Using Complex Variables," Proc., 14th AIAA Computational Fluid Dynamics Conference, AIAA Paper No. 993294, June 1999.

Janus, J. M., Horstman, H. S., and Whitfield, D.L., "Unsteady Flowfield Simulation of Ducted PropFan Configurations," Journal of Propulsion and Power, Vol. 15, No. 1, JanuaryFebruary 1999, pp. 6472.

Arabshahi, A. and Janus, J. Mark, "A Multiblock Compressible NavierStokes Flow Solver Applied to Complex Launch Vehicles," AIAA993378, June 28  July 1, 1999.

Sheng, C., Hyams, D., Sreenivas, K., Gaither, J.A., Marcum, D. L., Whitfield, D.L. and Anderson, W.K., "ThreeDimensional Incompressible NavierStokes Flow Computations About Complete Configurations Using a MultiBlock Unstructured Grid Approach," AIAA990778, 37th AIAA Aerospace Sciences Meeting, Reno, NV, January 1999.

Arabshahi, A., Janus, J. M., “ A Multiblock Compressible NavierStokes Flow Solver Applied to Complex Launch Vehicles,” AIAA993378, the 14th Computational Fluid Dynamics Conference, Norfolk, VA, June 1999.

Arabshahi, A., Gibeling H. J., “Computational Hydrodynamics for Autonomous Underwater Vehicles,” the 4th Mississippi State Conference on Differential Equations & Computational Simulations, May 1999.

Thomas, J. L., Bonhaus, D. L., Anderson, W. K., Rumsey, C. L., and Biedron, R. T., "An 0(Nm^2) Plane Solver for the Compressible NavierStokes Equations," AIAA 990785, January, 1999.

Anderson, W. K., and Bonhaus, D. L., "Airfoil Design on Unstructured Grids for Turbulent Rows," AIAA Journal, Vol. 37, No. 2, Feb. 1999, pp. 185191.

Sheng, C., Whitfield, D. L., and Anderson, W K., "Multiblock Approach for Calculating Incompressible Fluid Rows on Unstructured Grids," AIAA Journal, Vol. 37, No. 2, Feb. 1999, pp. 169176.

Nielsen, E. J., Anderson, W. K., and Kaushik, D. K., "Implementation of a Parallel Framework for Aerodynamic Design Optimization on Unstructured Meshes," Presented at the 11th International Parallel CFD Conference, Williamsburg, Va., May 1999.

Nielsen, E. J., Anderson, W K., "Aerodynamic Design Optimization on Unstructured Meshes Using the NavierStokes Equations," AIAA Journal, Vol. 37, No. 11, Nov. 1999, pp. 14111419.

Anders, J. B., Anderson, W. K., and Murthy, A. V, "Transonic Similarity Theory Applied to a Supercritical Airfoil in Heavy Gas" J. of Aircraft, Vol. 36, No. 6, Nov. 1999, pp. 957964.

Anderson, W Kyle, and Venkatakrishnan, V, "Aerodynamic Design Optimization on Unstructured Grids with a Continuous Adjoint Formulation," Computers and Fluids, Vol. 28, No. 45, 1999, pp.443480.

Anderson, W K., Gropp, W D., Kaushik, D. K., Keyes, D. E., and Smith, B. F, Proceedings of Supercomputing '99, 1999. Winner of Gordon Bell Prize, 1999.

Demuren A., Wilson R., “Streamwise Vorticity Generation in Laminar and Turbulent Jets”, Proceedings of the 3rd ASME/JSME Joint Fluids Engineering Conference, FEDSM996807, San Francisco, July 1823, 1999.

Stern F., Wilson R., Coleman H., and Paterson E., “Verification and Validation of CFD Simulations”, Proceedings of the 3rd ASME/JSME Joint Fluids Engineering Conference, FEDSM996913, San Francisco, July 1823, 1999.

Eglin J. L., GravesBrook, M. K., "Reactivity of the Re2(III,III) core with substituted nitriles," Abstracts of Papers, 218th ACS National Meeting, August 2226 (1999).
1998 (back to top)

Beddhu, M., Nichols, S., Jiang, M.Y., Sheng, C., Whitfield, D.L., and Taylor, L.K., "Comparison of EFD and CFD Results of the Free Surface Flow Field about the Series 60 Cb = O.6 Ship," 25th American Towing Conference, Iowa City, IA, Sept. 1998.

Arabshahi, A., Beddhu, M., Briley, W.R., Chen, J.P., Gaither, A., Gaither, K., Janus, J.M., Jiang, M., Marcum, D., McGinley, J., Pankajakshan, R., Remotigue, M., Sheng, C., Sreenivas, K., Taylor, L.K., and Whitfield, D.L., "A Perspective on Naval Hydrodynamic Flow Simulations," Presented at the 22nd Symposium on Naval Hydrodynamics, Washington, D.C., August 914, 1998.

Beggs, J. H., and W. R. Briley, "An Implicit Characteristic Based Method for Computational Electromagnetics," Report MSSUCOEERC9811, August, 1998. Submitted to J. Applied Computational Electromagnetics Society.

Newman, J.C., Anderson, W.K., and Whitfield, D.L., "Multidisciplinary Sensitivity Derivatives Using Complex Variables," MSSUCOEERC9808, July 1998.

Whitfield, D.L., and Taylor, L.K., "Variants of a TwoLevel Method for the Approximate Numerical Solution of Field Simulation Equations," MSSUEIRSERC9809, July 1998.

Sreenivas, K. and Whitfield, D.L., "Timeand Frequencydomain Numerical Simulation of Linearized Euler Equations," AIAA Journal, Vol. 36, No. 6, June 1998, pp. 968975.

Taylor, L.K., Pankajakshan, R., Jiang, M., Sheng, C., Briley, W.R., Whitfield. D.L., Davoudzadeh, F., Boger, D.A., Gibeling, H.J., Gorski, J., Haussling, H., Coleman, R., and Buley G., "LargeScale Simulations for Maneuvering Submarines and Propulsors," AIAA Paper No. 982930, 29th AIAA Plasmadynamics and Lasers Conference, Albuquerque, NM, June 1518, 1998.

Beddhu, M., Jiang, M. Y., Whitfield, D. L., Taylor, L. K. and Arabshahi, A., "CFD Validation of the Free Surface Flow Around DTMB Model 5415 Using Reynolds Averaged NavierStokes Equations," Presented in the Third Osaka Colloquium on Advanced CFD Applications to Ship Flow and Hull Form Design, Osaka, Japan, May 2527, 1998.

Busby, J.A., Taylor, L. K., Jiang, M.Y., and Whitfield, D.L., "Unsteady 3D Incompressible Flow Interaction in Multiple BladeRow Turbomachinery," AIAA Paper No. 980423, AIAA 36th Aerospace Sciences Meeting and Exhibit, Reno, NV, January 1215, 1998.

Beddhu, M., Jiang, MY., Taylor, L.K., and Whitfield, D.L., "Computation of Steady and Unsteady Flows with a Free Surface Around the Wigley Hull," Applied Mathematics and Computation, Vol. 89, pp. 6784, 1998.

Arabshahi, A., et. al., “A Perspective on Naval Hydrodynamic Flow Simulations,” The 22nd Naval Hydrodynamics Program, August 1998.

Beddhu, M., Jiang, M. Y., Whitfield, D. L., Taylor, L. K., and Arabshahi, A., “An Algorithm for Calculating Unsteady Free Surface Flows Around Complex Geometries Using Reynolds Average NavierStokes Equations.” Submitted for publication in Journal of Computational Physics, April 1998.

Webster, R. S., ‘‘Numerical Study of Base Flow Induced by Exhaust Plume Impingement’’, AIAA983621, July, 1998.

Nichols, D. S. III, "Calculation of Free Surface Wave Forms and Flow Field about the Series 60 CB = 0.6 Ship," Masters Thesis, Mississippi State University, May 1998.

Wilson R., Demuren A., “Numerical Simulation of Turbulent Jets with Rectangular CrossSection”, Journal of Fluids Engineering, 120, June 1998, pp. 285290.

Wilson R., Paterson E., Leighton R., Longo J., and Stern F., “Unsteady Modeling of a Naval Combatant in Head Waves: RANS CFD and EFD”, Proceedings of 22nd Symposium on Naval Hydrodynamics, Washington D.C., August 914, 1998.

Wilson R. and Demuren A., “On the Origin of Streamwise Vorticity in Complex Turbulent Jets”, Proceedings of the ASME Fluids Engineering Division Summer Meeting, FEDSM985004, Washington D.C., June 2125, 1998.

Paterson E., Wilson R., and Stern F., “Verification/Validation of Steady Flow RANS CFD for Naval Combatant”, Proceedings of 1st Symposium on Marine Applications of Computational Fluid Dynamics, Washington D.C., May 1998.

Eglin, J. L., GravesBrook, M. K., Concolino, T. E., Staples, R. J., "Studies of the reactivity of dirhenium complexes with isocyanides," Book of Abstracts, 215th ACS National Meeting, March 29April 2 (1998).
1997 (back to top)

Pankajakshan, R., "Parallel Solution of Unsteady Incompressible Viscous Flows using Multiblock Structured Grids," Ph.D. Dissertation, Mississippi State University, Dec. 1997.

Pankajakshan, R., Briley, W.R., Taylor, L.K., Sheng, C., Jiang, M.Y., and Whitfield, D.L., "Parallel Simulation Methodology for Maneuvering Submarine/Propulsor Configurations," Maneuvering Submarine Review, NSWC/Carderock, October 1997.

Sheng, C., Whitfield, D.L. and Anderson, W.K., "A Multiblock Approach for Calculating Incompressible Fluid Flows on Unstructured Grids," AIAA Paper No. 971866, 13th AIAA Computational Fluid Dynamics Conference, Snowmass, CO, June 1997.

Beddhu, M., Jiang, M. Y., Whitfield, D. L., Taylor, L. K. and Arabshahi, A., "An Algorithm for Calculating Unsteady Free Surface Flows Around Complex Geometries Using Reynolds Averaged NavierStokes Equations," Presented at the ONR Ship Hydrodynamics Workshop, David Taylor Model Basin, Carderock, MD, June 23, 1997.

Davoudzadeh, F., Taylor, L. K., Zierke, W. C., Dryer, J. J., McDonald, H. and Whitfield, D. L., "Coupled NavierStokes and Equations of Motion Simulation of Submarine Maneuvers, Including Crashback," FEDSM973129, 1997 ASME Fluids Engineering Division Summer Meeting, Vancouver, British Columbia, Canada, June 2226, 1997.

Dryer, J. J., Taylor, L. K., Zierke, W. C. and Davoudzadeh, F., "A FirstPrinciple Approach to the Numerical Prediction of the Maneuvering Characteristics of Submerged Bodies," FEDSM973130, 1997 ASME Fluids Engineering Division Summer Meeting, Vancouver, British Columbia, Canada, June 2226, 1997.

Beddhu, M., Jiang, MY., Whitfield, D.L., Taylor, L.K., and Arabshahi, A., "Computational Physical Oceanography A Comprehensive Approach Based on Generalized CFD/Grid Techniques for Planetary Scale Simulations of Oceanic Flows," MSSUEIRSERC975, March 1997.

Briley, W. R., and Hodge, B. K., "A CFD Project Combining Solution Algorithms, Software Development/Validation and Viscous Flow Calculations," Computer Applications in Engineering Education, Vol. 5, No. 3, pp. 161168, 1997.

Chen, J. P., Ghosh, A. R., Sreenivas, D., and Whitfield, D. L., "Comparison of Computations Using NavierStokes Equations in Rotating and Fixed Coordinates for Flow Through Turbomachinery," AIAA Paper No. 970878, AIAA 35th Aerospace Sciences Meeting and Exhibit, Reno, NV, January 610, 1997.

Jonnalagadda, R., Taylor, L. K., and Whitfield, D. L., "Multiblock Multigrid Incompressible RANS Computation of Forces and Moments on Appended SUBOFF Configurations at Incidence," AIAA Paper No. 970624, AIAA 35th Aerospace Sciences Meeting and Exhibit, Reno, NV, January 610, 1997.

Sheng, C., Chen, J.P., Taylor, L. K., Jiang, M.Y., and Whitfield, D.L., "Unsteady Multigrid Method for Simulating 3D Incompressible NavierStokes Flows on Dynamic Relative Motion Grids," AIAA Paper No. 970446, AIAA 35th Aerospace Sciences Meeting and Exhibit, Reno, NV, January 610, 1997.

Boger, D.A., Davoudzadeh, F., Dreyer, J.J., McDonald, H., Schott, C.G., Zierke, W.C., Arabshahi, A., Briley, W.R., Busby, J.A., Chen, J.P., Jiang, M.Y., Jonnalagadda, R., McGinley, J., Pankajakshan, R., Sheng, C., Stokes, M.L., Taylor, L.K., and Whitfield, D.L., "A PhysicsBased Means of Computing the Flow Around a Maneuvering Underwater Vehicle," Technical Report No. TR 97002, Applied Research Laboratory, Penn State University, January 1997.

Razzaghi, M., Arabshahi, A., and Lin, S. D., “Analysis of Linear Distributed Parameter Systems via Double Fourier Series,” Applied Mathematics and Computation, Vol. 87, No. 23, pp. 205215, 1997.

Reed, C.L., Karman, Jr., S.L., “Implementation of Low Speed Preconditioning in the Splitflow Code”, AIAA 971867, 1997.

Wilson R. and Demuren A., “LargeEddy Simulation of Complex Turbulent Jets”, Proceedings of ASME Fluids Engineering Division Summer Meeting, FEDSM975214, Vancouver BC, Canada, June 1997.
1996 (back to top)

Beddhu, M., Taylor, L. K., and Whitfield, D. L., "Strong Conservative Form of the Incompressible NavierStokes Equations in Rotating Frame with a Solution Procedure," Journal of Computational Physics, Vol. 128, No. 2, October 1996, pp. 427437.

Whitfield, D. L., "Numerical Solution of the Shallow Water Equations," MSSUEIRSERC964, July 1996.

McDonald, H. and Whitfield, D. L., "SelfPropelled Maneuvering Underwater Vehicles," TwentyFirst Symposium on Naval Hydrodynamics, Trondheim, Norway, June 2428, 1996.

Pankajakshan, R. and W. R. Briley, "Parallel Solution of Viscous Incompressible Flow on MultiBlock Structured Grids Using MPI," Parallel Computational Fluid Dynamics  Implementations and Results Using Parallel Computers, Edited by S. Taylor, A. Ecer, J. Periaux, and N. Satofuca, Elsevier Science, B. V., Amsterdam, pp. 601608, 1996.

Briley, R., Neerarambam, S.S., and Whitfield, D.L., "Implicit LowerUpper/Approximate Factorization Algorithms for Incompressible Flows," Journal of Computational Physics, Vol. 123, March 1996, pp. 3242.

Sheng, C., Taylor, L.K., Chen, J.P, Jiang, M.Y., and Whitfield, D.L., "Multigrid Computations of 3D Incompressible Internal and External Viscous Rotating Flows," MSSUEIRSERC961, February 1996.

Finley, D.B., Karman Jr., S.L., "Prediction of Compressibility Effects Using Unstructured Euler Analysis on Vortex Dominated Flow Fields," AIAA 962499, 1996.

Wilson R., Demuren A., “Numerical Simulations of TwoDimensional, Spatially Developing Mixing Layers”,Numerical Heat Transfer, Part A, 29, 1996, pp. 485509.

Wilson R. and Demuren A., “Numerical Simulation of Turbulent Jets with Rectangular CrossSection”, Proceedings of the ASME Fluids Engineering Division Summer Meeting, FEDVol. 238(3), San Diego, California, July 1996, pp. 121128.
1995 (back to top)

Sheng, C., Taylor, L. K., and Whitfield, D. L., "Multigrid Algorithm for ThreeDimensional Incompressible HighReynolds Number Turbulent Flows," AIAA Journal, Vol. 33, No. 11, November 1995, pp. 20732079.

Taylor, L. K. and Whitfield, D. L., "Investigation of the Accuracy of an Unsteady Incompressible Euler Equation Algorithm," Proceedings of the International Conference on Scientific Computing and Modeling, Eastern Illinois University, October 1995.

Arabshahi, A. and Whitfield, D. L., "Multiblock Euler Computation of Transonic Flow About a Generic Aircraft Configuration," International Journal of Computational Fluid Dynamics, Vol. 4, Numbers 34, September 1995, ISSN: 1061 8562 IJCCFEC, pp. 307321.

Sheng, C., Taylor, L. K., and Whitfield, D. L., "A Multigrid Algorithm for Unsteady Incompressible Euler and NavierStokes Flow Computations," Sixth International Symposium on Computational Fluid Dynamics, Lake Tahoe, Nevada, September 48, 1995.

Briley, W. R., Neerarambam, S. S., and Whitfield, D. L., "Implicit LowerUpper/Approximate Factorization Algorithms for Viscous Incompressible Flows," AIAA Paper No. 951742  CP, 12th Computational Fluid Dynamics Conference, San Diego, CA, June 1922, 1995.

Vanden, K. J. and Whitfield, D. L., "Direct and Iterative Algorithms for the ThreeDimensional Euler Equations,"AIAA Journal, Vol. 33, No. 5, May 1995, pp. 851858.

Beddhu, M., Jiang, MY., Taylor, L.K., and Whitfield, D.L., "Computation of Steady and Unsteady Flows with a Free Surface Around the Wigley Hull," Mississippi State Annual Conference on Differential Equations and Computational Simulations, Mississippi State, MS, April 1995.

Webster, R. S., Chen, J. P., and Whitfield, D. L., "Numerical Simulation of a Helicopter Rotor in Hover and Forward Flight," AIAA Paper No. 950193, AIAA 33rd Aerospace Sciences Meeting and Exhibit, Reno, NV, January 912, 1995

Taylor, L. K., Arabshahi, A., and Whitfield, D. L., "Unsteady ThreeDimensional Incompressible NavierStokes Computations for a 6:1 Prolate Spheroid Undergoing TimeDependent Maneuvers," AIAA Paper No. 950313,AIAA 33rd Aerospace Sciences Meeting and Exhibit, Reno, NV, January 912, 1995.

Arabshahi, A., Taylor, L. K., and Whitfield, D. L., "UNCLE: Toward a Comprehensive TimeAccurate Incompressible NavierStokes Flow Solver," AIAA Paper No. 950050, AIAA 33rd Aerospace Sciences Meeting and Exhibit, Reno, NV, January 912, 1995.

Sheng, C., Taylor, L. K., and Whitfield, D. L., "Multiblock Multigrid Solution of ThreeDimensional Incompressible Turbulent Flow About Appended Submarine Configurations," AIAA Paper No. 950203, AIAA 33rd Aerospace Sciences Meeting and Exhibit, Reno, NV, January 912, 1995.

Whitfield, D. L., "Perspective on Applied CFD," AIAA Paper No. 950349, AIAA 33rd Aerospace Sciences Meeting and Exhibit, Reno, NV, January 912, 1995.

Razzaghi, M., Arabshahi, A., and Lin, S. D., “Identification of Nonlinear Differential Equations Via Fourier Series Operational Matrix for Repeated Integration,” Applied Mathematics and Computation, Vol. 68, pp. 189198, 1995.

Daiber, M.P., Bomba, Joseph, and Swafford, T.W., “Analysis Method for the Design of Compensated Pitotstatic Probes for Use on General Aviation Aircraft,” SAE Technical Paper 951431, 1995 SAE Aerospace Atlantic Conference, May 2325, 1995, Dayton, Ohio.

Swafford, T.W., Bomba, Joseph, and Daiber, M.P., “Computational Analysis of Compensated Pitotstatic Probes Using the Euler Equations,” AIAA951839CP, AIAA Applied Aerodynamics Conference, San Diego, California, June 1995.

Karman, Jr., S.L., “SPLITFLOW: A 3D Unstructured Cartesian/Prismatic Grid CFD Code for Complex Geometries,” AIAA 950434, 1995.

Welterlen, T.J., Karman, Jr., S.L., “Rapid Assessment of F16 Store Trajectories Using Unstructured CFD,” AIAA 950354, 1995.

Karman, Jr., S.L., “Unstructured Cartesian/Prismatic Grid Generation for Complex Geometries,” NASA Conference Publication 3291, “Surface Modeling, Grid Generation, and Related Issues in Computational Fluid Dynamics,” 1995.

Melnik, R. E., "An Overview of a Recent Industry Effort at CFD Code Certification," presented at the 26 th AIAA Fluid Dynamics Conference, San Diego, CA, AIAA Paper No. 952229, June, 1995 (coauthor)
1994 (back to top)

Arabshahi, A., and Pankajakshan, R., “Propulsion/Airframe Interference for Ducted Propfan Engines with Ground Effect,” NASACR197110, November 1994.

Beddhu, M., Taylor, L.K., and Whitfield, D.L., "A Time Accurate Calculation Procedure for Flows with a Free Surface Using a Modified Artificial Compressibility Formulation," Applied Mathematics and Computation, Vol. 65, pp. 3348, 1994.

Beddhu, M, Jiang, MY., Taylor, L. K., and Whitfield, D. L., "Toward Computation of Ocean Flows Using NavierStokes Equations," Supercomputing '94 Proceedings, IEEE Computer Society Press, 1994, pp. 144153.

Whitfield, D. L., Taylor, L. K., Beddhu, M., and Arabshahi, A., "Discretized NewtonRelaxation Solution of the Threedimensional Unsteady Incompressible NavierStokes Equations," Frontiers of Computational Fluid Dynamics, Chapter 28, pp. 575594, D.A. Caughey and M. M. Hafez editors, Wiley Publishing, 1994.

Sheng. C., Taylor, L., and Whitfield, D. L., "An Efficient Multigrid Acceleration for Solving the 3D Incompressible NavierStokes Equations in Generalized Curvilinear Coordinates," AIAA942335, 25th AIAA Fluid Dynamics Conference, Colorado Springs, CO, June 1994.

Chen, J. P., and Whitfield, D.L., "CFD Code Assessment Sessions," 39th ASME International Gas Turbine and Aeroengine Congress, The Hague, The Netherlands, June 1994.

Hyams, D. G., and Fadel, G. M., "Comparison of Various Move Limit Strategies in Structural Optimization," AIAA Paper 941359, 35th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, Hilton Head, SC, April 1820, 1994.

Whitfield, D. L. and Taylor, L. K., "Numerical Solution of the TwoDimensional TimeDependent Incompressible Euler Equations," MSSUEIRSERC9314, April 1994.

Swafford, T.W., Loe, D.H., Huff, D.L., Huddleston, D.H., and Reddy, T.S.R., “The Evolution of NPHASE: Euler/NavierStokes Computations of Unsteady Two Dimensional Cascade Flow Fields,” AIAA941834CP, June 1994.

Webster, R.S., "Numerical Simulation of a Helicopter Rotor in Hover and Forward Flight", M.S. Thesis, Mississippi State University, August 1994. Melnik, R. E., "A process for Industry Certification of Physical Simulation Codes," presented at the 25 th Fluid Dynamics Conference, Colorado Springs, Colorado, AIAA Paper No. 942235, July, 1994 (coauthor)

Demuren A., Wilson R., “Estimating Uncertainty in Computations of TwoDimensional Separated Flows”, Journal of Fluids Engineering, 216, June 1994, pp. 216220.
1993 (back to top)

Arabshahi, A. and Whitfield, D. L., "Numerical Simulation of Supersonic Unsteady Flow for Multibody Configuration," International Journal of Scientific Computing and Modeling, Vol. 1, Special Issue, December 1993, pp. 111126.

Taylor, L. K., Busby, J. A., Jiang, M. Y., Arabshahi, A., Sreenivas, K., and Whitfield, D. L., "Time Accurate Incompressible NavierStokes Simulation of the Flapping Foil Experiment," Proceedings of the Sixth International Conference on Numerical Ship Hydrodynamics, Iowa City, Iowa, August 25, 1993, pp. 721738.

Sreenivas, K., Whitfield, D.L., and Huff, D.L., "High Resolution Numerical Simulation of the Linearized Euler Equations in Conservation Law Form," AIAA Paper No. 932934, AIAA 24th Fluids Dynamics Conference, Orlando, FL, July 69, 1993.

Vanden, K. J. and Whitfield, D.L., "Direct and Iterative Algorithms for the ThreeDimensional Euler Equations," AIAA Paper No. 933378, 11th AIAA Computational Fluid Dynamics Conference, Orlando, FL, July 69, 1993.

Pankajakshan, R., Arabshahi, A., and Whitfield, D.L., "Turbofan Flowfield Simulation Using Euler Equations with Body Forces," AIAA Paper No. 931978, AIAA/SAE/ASME/ASEE 29th Joint Propulsion Conference and Exhibit, Monterey, CA, June 2830, 1993.

Beddhu, M., Taylor, L.K., and Whitfield, D.L., "A Time Accurate Calculation Procedure for Incompressible Flows with a Free Surface Using a Modified Artificial Compressibility Formulation," Mississippi State Annual Conference on Differential Equations and Computational Simulations, Mississippi State, MS, March 1993.

Cox, C. F., Cinnella, P., and Arabshahi, A., “MultiBlock Calculation for Flows in Local Chemical Equilibrium,” AIAA932999, 24th AIAA Fluid Dynamics Conference, Orlando, FL, July 1993.

Hammersley, J. R., Olson, D. E., Reddy, R. N., Arabshahi, A., and Gatlin, B., “Computational Modeling of Airflows in the Smaller Airways,” American Review of Respiratory Diseases, Vol. 145, p. A32, April 1993.

Soni, B. K., Huddleston, D. H., Arabshahi, A., and Vu, B., “A Study of CFD Algorithms Applied to Complete Aircraft Configurations,” AIAA930784, AIAA 31st Aerospace Sciences Meeting, Reno, NV, January 1993.

Swafford, T.W., “Computation of Unsteady Supersonic QuasiOneDimensional ViscousInviscid Interacting Flow Fields,” AIAA Journal, Vol. 31, No. 2, pp. 404408, February 1993.

Melnik, R. E., "Applications of a new WallSlip Boundary Condition to the computation of Turbulent Flows," presented at the AIAA 24th Fluid Dynamics Conference, Orlando, Fl, AIAA paper No. 933108, July, 1993, (coauthor)

Wilson R. and Demuren A., “Estimating Uncertainty in Computations of TwoDimensional Separated Flows”, Proceedings of the Quantification of Uncertainty in Computational Fluid Dynamics, FEDVol 158, Washington D.C., June 1993, pp. 918.

Wilson R., “On the Prediction of Multigrid Efficiency Through Local Mode Analysis”, Proceedings of Sixth Copper Mountain Conference on Multigrid Methods, Part 2, eds. N. Melson, T. A. Manteuffel, and S. F. McCormick, NASA Langley Research Center, Hampton, Va. 1993, pp. 679689.
1992 (back to top)

Whitfield, D. L., "An Implicit Solution of Roe's Approximate Riemann Solver Using True and Approximate Jacobians, Including Discretized and Sparse Matrix Updating," Engineering & Industrial Research Station Report, MSSUEIRSERC931, Mississippi State University, Mississippi State, MS, October 1992.

Janus, J.M., Arabshahi, A., and Whitfield, D.L., "Numerical Solution and Algorithm Analysis for the Unsteady NavierStokes Equations on Dynamic Multiblock Grids, Volume I," WLTR927044, Eglin Air Force Base, FL, October 1992.

Janus, J.M., Cox, C.F., Arabshahi, A., Cinnella, P. C., and Whitfield, D.L., "Numerical Solution and Algorithm Analysis for the Unsteady NavierStokes Equations on Dynamic Multiblock Grids Including Chemical Equilibrium, Volume II," WLTR927044, Eglin Air Force Base, FL, October 1992.

Mansfield, F. A. and Whitfield, D. L., "Investigation of Solution Operators for the ThreeDimensional Unsteady Euler Equations," AIAA Paper No. 922666, June 1992.

Buggeln, R. C., Shamroth, S. J. and Briley, W. R., "Development of a Dynamic Lift Analysis," SRA Report R92920043F, NASA Contract N0001991C0088, 1992.

Simpson, L. B. and Whitfield, D. L., "FluxDifference Split Algorithm for Unsteady ThinLayer NavierStokes Solutions," AIAA Journal, Vol. 30, No. 4, April 1992, pp. 914922.

Janus, J. M., Horstman, H. Z., and Whitfield, D. L., "Unsteady Flowfield Simulation of Ducted PropFan Configurations," AIAA Paper No. 920521, January 1992.

Mansfield, F. A. and Whitfield, D. L., "Investigation of Solution Operators for the TwoDimensional Unsteady Euler Equations," AIAA Paper No. 920050, January 1992.

Janus, J.M., Cox, C.F., Arabshahi, A., Cinnella, P., and Whitfield, D.L., "Numerical Solution and Algorithm Analysis for the Unsteady NavierStokes Equations on Dynamic Multiblock Grids Including Chemical Equilibrium," Vol. 2, Report No. WLTR927044, Wright Laboratory, 1992.

Hammersley, J. R., Reddy, R. N., and Arabshahi, A., “Computational Simulation of Airflow Within Human Lungs,” Arkansas Computer Science Conference, Little Rock, AR, October 1992.

Hammersley, J. R., Olson, D. E., Reddy, R. N., Arabshahi, A., and Gatlin, B., “Computational Modeling of Airflows in the Smaller Airways,” American Lung Association Conference, Miami Beach, FL, May 1992.

Thompson, B.E., Senald, J., Vafidis, C., Whitelaw, J.H., McDonald, H., “Flow in a model of the Space Shuttle Main Engine main injector bowl,” AIAA Journal of Spacecraft and Rockets, vol. 29, (MarApr 1992), p. 247252.

Liu, N.S., Shamroth, S.J., McDonald, H., “Reciprocal interactions of hairpinshaped vortices and a boundary layer,” AIAA Journal, vol. 29, (May 1992), p. 720727.

Reddy, T.S.R., Bakhle, Milind A., Huff, Dennis L., and Swafford, T.W., “Flutter Analysis of Supersonic Axial Flow Cascades Using a High Resolution Euler Solver; Part I: Formulation and Validation,” NASA Technical Memorandum 105798, August 1992 (Limited Distribution Until August 1994).

Swafford, Timothy W., Huddleston, David H., Busby, Judy A., and Chesser, B. Lawrence, “Computation of Steady and Unsteady QuasiOneDimensional ViscousInviscid Interacting Internal Flows at Subsonic, Transonic, and Supersonic Mach Numbers,” Mississippi State University, Engineering and Industrial Research Station ReportMSSUEIRSERC921, June 1992.

Reddy, T.S.R., Bakhle, Milind A., Huff, D.L., and Swafford, T.W., “Analysis of Cascades Using a Two Dimensional Euler Solver,” AIAA922370, April 1992.
1991 (back to top)

Taylor, L. K. and Whitfield, D. L., "Unsteady ThreeDimensional Incompressible Euler and NavierStokes Solver for Stationary and Dynamic Grids," AIAA Paper No. 911650, June 1991.

Whitfield, D. L. and Taylor, L. K., "Discretized NewtonRelaxation Solution of High Resolution FluxDifference Split Schemes," AIAA Paper No. 911539, June 1991.

Govindan, T. R., Briley, W. R., and McDonald, H., "General ThreeDimensional Viscous Primary/Secondary Flow Analysis," AIAA Journal, Vol. 29, No. 3, pp. 361390, 1991.

Briley, W. R., Roscoe, D. V., Gibeling, H. J., Buggeln, R. C. and Sabnis, J. S., "Computation of Flow Past a Turbine Blade With and Without Tip Clearance," presented at 36th ASME International Gas Turbine and Aeroengine Congress and Exposition (Orlando, FL), June 1991.

Govindan, T. R. and Briley, W. R., "Generalized Primary/Secondary Flow Analysis of Viscous Flow Around Bodies at Incidence," AIAA Paper No. 910186 (29th Aerospace Sciences Meeting, Reno, NV), 1991.

Arabshahi, A. and Whitfield, D. L., “Numerical Simulation of Supersonic Unsteady Flow for Multibody Configuration,” AIAA910023, AIAA 29th Aerospace Sciences Meeting and Exhibit, Reno, NV, January 1991.

Razzaghai, M. and Arabshahi, A., “Solutions of Convolution Integral and Fredholm Integral Equation Via Double Fourier Series,” Applied Mathematics and Computation, Vol. 40, No. 3, pp. 215224, 1991.

Reddy, T.S.R., Bakhle, Milind A., Huff, D.L., and Swafford, T.W., “Flutter Analysis of Cascades Using a Two Dimensional Euler Solver,” AIAA911681, June 1991.

Huff, D.L., Swafford, T.W., and Reddy, T.S.R., “Euler Flow Predictions for An Oscillating Cascade Using a High Resolution WaveSplit Scheme,” ASME91GT198, June 1991.

Swafford, T.W., Unsteady ViscousInviscid Interaction via Direct Coupling of the 1D Euler and 2D Integral BoundaryLayer Equations,” Mississippi State University, Engineering and Industrial Research Station ReportMSSUEIRSERC901, March 1991.

Karman, Jr., S.L., Spragle, G.S., “Development of an Unstructured CFD Method,” AIAA 910019, 1991.

Karman, Jr., S.L., “Development of a 3D Unstructured CFD Method,” Ph.D. Dissertation, May 1991, University of Texas at Arlington.

Karman, Jr., S.L., Spragle, G.S., “Calibration of 2D Unstructured Grid Methods on Propulsive Flowfields,” AGARD Fluid Dynamics Panel Symposium on “Aerodynamic EngineAirframe Integration,” Paper No. 27, October, 1991.

Melnik, R. E., "Some Applications of Asymptotic Theory to Turbulent Flow," presented at the 29th Aerospace Sciences Meeting, Reno, Nevada, AIAA Paper No. 910220, January,1991.

Melnik, R. E., "NavierStokes Computations of Turbulent Flows Using a New Wall Boundary Condition," presented at the 4th International Symposium on Computational Fluid Dynamics at the University of California at Davis, CA September,1991, (coauthor).
1990 (back to top)

Whitfield, D. L., "NewtonRelaxation Schemes for Nonlinear Hyperbolic Systems," Engineering & Industrial Research Station Report, MSSUEIRSASE903, Mississippi State University, Mississippi State, MS, October 1990.

Janus, J. M., Whitfield, D. L., Horstman, H., and Mansfield, F., "Computation of the Unsteady Flowfield About a Counter Rotating Propfan Cruise Missile," AIAA Paper No. 903093, August 1990.

Liu, N. S., Davoudzadeh, F., Briley, W. R. and Shamroth, S. J., "NavierStokes Simulation of Transonic BladeVortex Interactions," Journal of Fluids Engineering, Vol. 112, pp. 501509, 1990.

Briley, W. R., Govindan, T. R. and McDonald, H, "Efficient Navier Stokes Flow Prediction Algorithms," SRA Report R90 900068 F, 1990.

DeJong, F.J., Sabnis, J.S., Buggeln, R.C., McDonald, H., “Hypersonic Flow Calculations with a Hybrid NavierStokes/Monte Carlo Method,” AIAA paper 901691. AIAA/ASME 5th Thermophysics and Heat Transfer Conference, Seattle, WA, June 1990, p. 15.

Liu, N.S., Shamroth, S.J., McDonald, H., “Reciprocal Interactions of HairpinShaped Vortices and a Boundary Layer,” AIAA Paper No. 900017, AIAA, 28th Aerospace Sciences Meeting, Reno, NV, January 1990, p. 11.

Govindan, T.R., DeJong, F.J., Briley, W.R., McDonald, H., “Rotating Flow in Radial Turbomachinery," Scientific Research Associates, Report No. ADA222885; SRAR930011F; ARO22360.4EGS, May 1990.
1989 (back to top)

Arabshahi, A. and Whitfield, D. L., "A Multiblock Approach to Solving the ThreeDimensional Unsteady Euler Equations About A WingPylonStore Configuration," AIAA Paper No. 893401, Presented at the AIAA Atmospheric Flight Mechanics Conference, Boston, MA, August 1416, 1989.

Simpson, L. B. and Whitfield, D. L., "A FluxDifference Split Algorithm for Unsteady ThinLayer NavierStokes Solutions," AIAA Paper No. 891995, June 1989.

Whitfield, D. L. and Thompson, J. F., "Computation of Transonic Flow About Stores," AFATLTR8920, Eglin Air Force Base, FL, June 1989.

Whitfield, D. L., Janus, J. M., and Arabshahi, A., "Unsteady Euler Solutions on Dynamic Blocked Grids for Complex Configurations," AGARD Specialists Meeting on Mesh Generation for Complex ThreeDimensional Configurations, Leon, Norway, May 2425, 1989.

Janus, J. M. and Whitfield, D. L., "A Simple TimeAccurate Turbomachinery Algorithm with Numerical Solutions of an Uneven Blade Count Configuration," AIAA Paper No. 890206, January 1989.

Whitfield, D. L., Janus, M. J., and Arabshahi, A., “Unsteady Euler Solutions on Dynamic Grids for Complex Configurations,” AGARDCP464, Loen, Norway, May 1989.

Arabshahi, A., “A Dynamic Multiblock Approach to Solving the Unsteady Euler Equations about Complex Configurations,” Ph.D. Dissertation, May 1989.

Razzaghi, M. and Arabshahi, A., “Solutions of Linear TwoPoint Boundary Value Problems Via Polynomial Series,”International Journal of Systems Science, Vol. 20, No. 3, pp. 375384, 1989.

Razzaghi, M., Tahai, A., and Arabshahi, A., “Solutions of TwoPoint Boundary Value Problems via Fourier Series and Application to Optimal Control of Linear Systems,” Journal of Franklin Institute, Vol. 326, No. 4, pp. 523533, 1989.

Razzaghi, M. and Arabshahi, A., “Optimal Control of Linear Distributed Parameter Systems via Polynomial Series,” International Journal of System Science, Vol. 20, No. 7, pp. 11411148, 1989.

Razzaghi, M. and Arabshahi, A., “Analysis of Linear TimeVarying Systems and Bilinear Systems Via Fourier Series,” International Journal of Control, Vol. 50, No. 3, pp. 889898, 1989.

Sabnis, J.S., Gibeling, H.J., McDonald, H., “NavierStokes analysis of solid propellant rocket motor internal flows,”Journal of Propulsion and Power, Vol. 5, (NovDec 1989), pp. 657664.

Thompson, B.E., Senaldi, J., Vafidis, C., Whitelaw, J.H., McDonald, H., “Flow in a Model of the SSME Main Injector Bowl,” Scientific Research Associates Report No. SE254832; Proceedings of the 1st Canadian Symposium of Aerodynamics, Ottawa, Canada, Dec 1989, Canadian Aeronautics and Space Institute, 1989, p. 301 to 3022

Sabnis, J.S., Madabhushi, R.K., Gibeling, H.J., McDonald, H., “On the Use of kEpsilon Turbulence Model for Computation of Solid Rocket Internal Flows,” AIAA Paper No. 892558, AIAA/ASME/SAE/ASEE 25th Joint Propulsion Conference, Monterey, CA, July 1989, p. 12.

Briley, W.R., Buggeln, R.C., McDonald, H., “Solution of the Incompressible NavierStokes Equations Using Artificial Compressibility Methods.” Proceedings of the 11th International Conference on Numerical Methods in Fluid Dynamics, Berlin and New York, SpringerVerlag, 1989, pp. 156160.

Clary, J.S., Howell, G.A., Karman, Jr., S.L., “Benchmark Calculations with an Unstructured Grid Flow Solver on a SIMD Computer,” Proceedings of the Supercomputing 1989 Conference, November 1989. IEEE Computer Society Order Number 2021.

Melnik, R. E., "An Asymptotic Theory of Turbulent of Turbulent Separation," Computers and Fluids, Vol.17, 1989
1988 (back to top)

Anderson, W. K., Thomas, J. L., and Whitfield, D. L., "ThreeDimensional Multigrid Algorithms for the FluxSplit Euler Equations," NASATP2829, November 1988.

Mounts, J. S., Belk, D. M., and Whitfield, D. L., "Program EAGLE User's Manual: Vol. IV  Multiblock Implicit, SteadyState Euler Code," AFATLTR88117, Vol. IV, Air Force Armament Laboratory, September 1988.

Briley, W. R., Buggeln, R. C. and McDonald, H., "Solution of the Incompressible Navier Stokes Equations Using Artificial Compressibility Methods," 11th International Conference on Numerical Methods in Fluid Dynamics (Williamsburg, VA), Springer Verlag, 1988.

Thompson, J. F. and Whitfield, D. L., "Transonic Flow Solutions on General 3D Regions Using CompositeBlock Grids," 11th International Conference on Numerical Methods in Fluid Dynamics, Williamsburg, VA, June 27  July 1, 1988.

Anderson, W. K., Thomas, J. L., and Whitfield, D. L., "Multigrid Acceleration of the FluxSplit Euler Equations,"AIAA Journal, Vol. 26, No. 6, June 1988, pp. 649654.

Janus, J. M. and Whitfield, D. L., "Improved 3D Turbomachinery CFD Algorithm," Final Report, Prepared for Scientific Research Associates, Inc., Glastonbury, CT, June 1988.

Pirzadeh, S. and Whitfield, D. L., "ThreeDimensional Unsteady Transonic ViscousInviscid Interaction Using the Euler and BoundaryLayer Equations," AIAA Paper No. 882578, June 1988.

Govindan, T. R., Briley, W. R. and Levy, R., "Computation of Flow Around Maneuvering Submerged Bodies. SRA Report R88 920029 F, 1988.

Whitfield, D. L., Janus, J. M., and Simpson, L. B., "Implicit Finite Volume High Resolution WaveSplit Scheme for Solving the Unsteady ThreeDimensional Euler and NavierStokes Equations on Stationary or Dynamic Grids,"Engineering and Industrial Research Station Report MSSUEIRSASE882, Mississippi State University, Mississippi State, MS, February 1988.

Roscoe, D.V., Buggeln, R.C., Foster, J.A., McDonald, H., “A Numerical Investigation of Fluid Flow for Disk Pumping Applications.” Proceedings of the ASME Gas Turbine and Aeroengine Congress and Exposition, Amsterdam, Netherlands, June 1988, p. 10.

Liu, N.S., Shamroth, S.J., McDonald, H., “Reciprocal interactions of HairpinShaped Vortices and a Boundary Layer,” Scientific Research Associates, Inc., Final Report, February 1, 1986 – December 31, 1988.

Liu, N.S., Shamroth, S.J., McDonald, H., “Flow Dynamics Stimulation by HairpinLike Vortices in Initially Laminar Boundary Layers.” Published in Scientific Research Associates, Inc., Annual Report, March 1988.
1987 (back to top)

Belk, D. M., Janus, J. M., and Whitfield, D. L., "ThreeDimensional Unsteady Euler Equations Solution on Dynamic Grids," AIAA Journal, Vol. 25, No. 9, September 1987, pp. 11601161.

Chen, H.C., Yu, H.J., Marcum, D.L., Kao, T.J., and Kusunose, K., "Coupled Euler/Boundary Layer Analysis of a Complete Aircraft with Viscous Modeling on the Lifting Surface," AIAA872614CP, 5th AIAA Applied Aerodynamics Conference, Monterey, CA, August 1987.

Belk, D. M. and Whitfield, D. L., "TimeAccurate Euler Equations Solutions on Dynamic Blocked Grids," AIAA Paper No. 871127CP, June 1987.

Gatlin, B. and Whitfield, D. L., "An Implicit Upwind Finite Volume Method for Solving the ThreeDimensional ThinLayer NavierStokes Equations," AIAA Paper No. 871149CP, June 1987.

Whitfield, D. L., Swafford, T. W., Janus, J. M., Mulac, R.A., and Belk, D. M., "ThreeDimensional Unsteady Euler Solutions for Propfans and CounterRotating Propfans in Transonic Flow," AIAA Paper No. 871197, June 1987.

Belk, D. M. and Whitfield, D. L., "3D Euler Solutions on Blocked Grids Using an Implicit TwoPass Algorithm," AIAA Paper No. 870450, January 1987.

Govindan, T.R., McDonald, H., “Computation of Tip and Corner Region Flows.” AGARD Computation of ThreeDimensional Boundary Layers Including Separation, February 1987, p. 20.

Sabnis, J.S., Gibeling, H.J., McDonald, H., “NavierStokes Analysis of Two and ThreeDimensional Flow Field in Solid Rocket Motors with Segment Joints.” AIAA/SAE/ASME/ASEE, 23rd Joint Propulsion Conference, San Diego, CA, July 1987, p. 11.

Sabnis, J.S., Gibeling, H.J., McDonald, H., “A Combined EulerianLagrangian Analysis for Computation of TwoPhase Flows.” AIAA Paper 871419, AIAA 19th Fluid Dynamics, and Lasers Conference, Honolulu, HI, June 1987, p. 10.

Buggeln, R. C., Briley, W.R., McDonald, H., Shamroth, S.J., Weinberg, B.C., “Two and ThreeDimensional Turbine Blade Row Flow Field Simulations,” Scientific Research Associates, Inc., SE254832. Published by NASA Lewis Research Center in Turbine Engine Hot Section Technology Report, October 1987, pp. 199209.

Sabnis, J.S., Gibeling, E.J., McDonald, H., “Solid Rocket Motor Aft Field Joint Flow Field Analysis,.” Published in Scientific Research Associates, Inc., Final Report, September 1987.

Chan, Y.T., Buggeln, R.C., McDonald, H., “ThreeDimensional Dynamic Labyrinth Seal Analysis,” Published in Scientific Research Associates, Inc., Final Report, January 1987, p. 50.

Liu, N.S., Shamroth, S.J., McDonald, H., “Flow Dynamics Stimulated by HairpinLike Vortices in Initially Laminar Boundary Layers.” Published in Scientific Research Associates, Inc., Annual Report, February 1987, p. 22.

Steinbrenner, J.P., Karman, Jr., S.L., Chawner, J.R., “Generation of Multiple Block Grids for Arbitrary 3D Geometries”, Printed in the AGARDOGRAPH on Mesh Generation, J. Steger and J. Thompson, coauthors, February, 1987.

Melnik, R. E., "A New Asymptotic Theory of Turbulent Boundary Layers and Its Application to Separation," Boundary Layer Separation, Springer Verlag, New York,1987.

Melnik, R. E., "An Overview of Computational Fluid Dynamics Development and Application at Grumman," presented at the NASA Conference on Supercomputing in Aerospace, 1012 March 1987.
1986 (back to top)

Janus, J. M. and Whitfield, D. L., "Advanced 3D Viscous SSME Turbine Rotor Stator CFD Algorithms," Final Report NAS836486, Prepared for George C. Marshall Space Flight Center, Marshall Space Flight Center, Alabama, September 1986.

Buggeln, R. C., Briley, W. R., Shamroth, S. J. and McDonald, H., "Solution of the Three Dimensional Navier Stokes Equations for Turbine Flows," 1st World Congress on Computational Mechanics (Univ. Texas, Austin TX), 1986.

Briley, W. R. and McDonald, H., "Accuracy and Iterative Convergence Rate of ADI Schemes for Scalar Convection," SRA Report R86 900050 F, 1986.

Belk, D. M., Janus, J. M., and Whitfield, D. L., "ThreeDimensional Unsteady Euler Equations Solutions on Dynamic Grids," AFATLTR8621, Air Force Armament Laboratory, April 1986.

Anderson, W. K., Thomas, J. L., and Whitfield, D. L., "Multigrid Acceleration of the Flux Split Euler Equations," AIAA Paper No. 860274, January 1986.

Kim, Y.N., Buggeln, R.C., McDonald, H., “Numerical Analysis of Some Supersonic Viscous Flows Related to Inlet and Nozzle Systems.” AIAA Paper 861597, AIAA/ASME/SAE/ASEE 22nd Joint Propulsion Conference, Huntsville, AL, June 1986, p. 13.

Brondum, D.C., Bennett, J.C., Weinberg, B.C., McDonald, H., “Numerical and Experimental Investigation of Nonswirling and Swirling Confined Jets.” AIAA 24th Aerospace Sciences Meeting, Reno, NV, January 1986, p. 15.

Buggeln R.C., Briley, W.R., Shamroth, S.J. and McDonald, H., "Solution of the Three Dimensional Navier Stokes Equations for Turbine Flows," 1st World Congress on Computational Mechanics, University of Texas, Austin, 1986.

Buggeln, R.C., Briley, W.R., Shamroth, S.J., McDonald, H., “Turbine Stator Flow Field Simulations,” Published by NASA Lewis Research Center in Turbine Engine Hot Section Technology Report, October 1986, pp. 233235.

Briley, W.R., Govindan, T.R., Levy, R., McDonald, H., “Numerical Study of ThreeDimensional Laminar and Turbulent Flows with System Rotation.” Published in Scientific Research Associates, Inc., Final Report, 1986, p. 46.

Gibeling, H.J., Weinberg, B.C., Shamroth, S.J., McDonald, H., “Flow Through a Compressor State,” Published in Scientific Research Associates, Inc., Final Report (Jun 1983 – May 1986), p. 55.

Buggeln, R.C., Kim, Y.N., McDonald, H., “Computation of MultiDdimensional Viscous Supersonic Flow,” Published in Scientific Research Associates, Inc., Final Report, (Oct. 1986), p. 194.

Kim, Y.N, Buggeln, R.C., McDonald, H., “Computation of MultiDimensional Viscous Supersonic Jet Flow,” Published in Scientific Research Associates, Inc., Final Report (Oct 1986), p. 128.

Weinberg, B.C., McDonald, H., “Influence of LargeScale Motion on Turbulent Transport for Confined Coaxial Jets. Volume 2: NavierStokes Calculation of Swirling and Nonswirling Confined Coaxial Jets,” Published in Scientific Research Associates, Inc., Final Report, January 1986, p. 57.

Buggeln, R.C., Briley, W.R., McDonald, H., “Solution of the ThreeDimensional Navier Stokes Equations for a Turbulent Horseshoe Vortex Flow,” Published in Scientific Research Associates, Inc. Final Report, October 1985 – September 1986, p. 36.

Briley, W.R. and McDonald, H., "Accuracy and Iterative Convergence Rate of ADI Schemes for Scalar Convection," SRA Report R86 900050 F, 1986.

Phares, W.J., Cooper, G.K., Swafford, T.W., and Jones, R.R., “Application of Computational Fluid Dynamics to Test Facility and Experiment Design,” AIAA861733, June 1986.

Karman, Jr., S.L., Steinbrenner, J.P., Kisielewski, K.M., “Analysis of the F16 Flow Field by a Block Grid Euler Approach,” AGARDCP412 Paper No. 18, Published November, 1986.

Reed, C.L., Karman, Jr., S.L., “MultipleBlock Grid Method Applied to Complex 3D Geometries,” Presented at Society for Industrial and Applied Mathematics 1986 National Meeting, July 1986, Boston, Mass. Unpublished.

Melnik, R. E., "Computation of Turbulent Separated Flow with an Integral Boundary Layer Method," paper presented at the 10th International Conference on Numerical Methods in Fluid Dynamics, Beijing, China, 2325 June 1986, published in Lecture Notes in Physics, 264, Springer Verlag, 1986 (coauthor).
1985 (back to top)

Lijewski, L. E., Thompson, J. F., and Whitfield, D. L., "Computational Fluid Dynamics for Weapon Carriage and Separation," AGARD Fluid Symposium on Store Airframe Aerodynamics, Athens, Greece, October 1985.

Edwards, D. E., Whitfield, D. L., and Carter, J. E., "Application of Interacting Boundary Layer Theory in the Analysis of Transonic Shock Induced Separation," International Union of Theoretical and Applied Mechanics (IUTAM), Palaiseau, France, September 1985.

Whitfield, D. L., "Implicit Upwind Finite Volume Scheme for the Three Dimensional Euler Equations," Engineering and Industrial Research Station Report MSSUEIRSASE851, Mississippi State University, Mississippi State, MS, September 1985.

Belk, D. M., Janus, J. M., and Whitfield, D. L., "ThreeDimensional Unsteady Euler Equations Solutions on Dynamic Grids," AIAA Paper No. 851704, July 1985.

Swafford, T. W. and Whitfield, D. L., "TimeDependent Solution of ThreeDimensional Compressible Turbulent Integral BoundaryLayer Equations," AIAA Journal, Vol. 23, No. 7, July 1985, pp. 10051013.

Whitfield, D. L., "ViscousInviscid Interaction Computations Using a Pseudo NavierStokes Approach," inNumerical and Physical Aspects of Aerodynamic Flows III, T. Cebeci, Editor, SpringerVerlag, New York, 1985.

Whitfield, D. L. and Thomas, J. L., "Transonic ViscousInviscid Interaction Using Euler and Inverse BoundaryLayer Equations," Vol. 3 of the Series in Recent Advances in Numerical Methods in Fluids entitled Computational Methods in Viscous Flow, W.G. Habashi, Editor, Pineridge Press, Swansea, U. K., 1985.

Briley, W. R., Buggeln, R. C. and McDonald, H., "Solution of the Three Dimensional Navier Stokes Equations for a Steady Laminar Horseshoe Vortex Flow," AIAA Paper No. 841520 CP, 7th CFD Conference (Univ. Cincinnati), 1985.

Lin, S. J., Briley, W. R. and McDonald, H., "Numerical Study of Three Dimensional Viscous Flows With System Rotation," AIAA Paper No. 851691 CP, (18th Fluid Dynamics and Plasmadynamics and Lasers Conference, Cincinnati OH), 1985.

Briley, W. R., McDonald, H. and Buggeln, R. C., "Observations on Three Dimensional Viscous Turbine Flow Analysis Methods," SRA Report R85 900029 F, 1985.

Liu, N.S., Shamroth, S.J., McDonald, H., “On Hairpin Vortices as Model of Wall Turbulence Structure,” Proceedings of the 5th Symposium on Turbulent Shear Flows, University Park, PA, 1985, p. 2.12.6.

Weinberg, B.C., Yang, R.J., McDonald, H., Shamroth, S.J., “Calculations of Two and ThreeDimensional Transonic Cascade Flow Fields Using the NavierStokes Equation,” ASME paper 85GT66, ASME 30th International Gas Turbine Conference and Exhibit, Houston, TX, March 1985, p. 10.

Roscoe, D.V., Gibeling, H.J., McDonald, H., Shamroth, S.J., “Development of a NavierStokes Analysis to Investigate the Mechanism of Shock/Wave Boundary Layer Interactions.” AIAA 3rd Symposium on Numerical and Physical Aspects of Aerodynamic Flows, Long Beach, CA, Jan. 1985, p.p. 415 – 423.

Briley, W.R., Buggeln, R.C., McDonald, H., “Solution of the ThreeDimensional NavierStokes Equations for a Steady Laminar Horseshoe Vortex Flow.” Proceedings of the AIAA 7th Computational Fluid Dynamics Conference, Cincinnati, OH, July 1985, pp. 299312.

Lin, S.J., Briley, W.R., McDonald, H., “Numerical Study of ThreeDimensional Viscous Flows with System Rotation.” AIAA 18th Fluid Dynamics and Plasmadynamics and Lasers Conference, Cincinnati, OH, July 1985, p. 13.

Sabnis J.S., Gibeling, H.J., McDonald, H., “Calculation of Solid Propellant Rocket Motor Internal Flow Field Using an Implicit NavierStokes Procedure.” AIAA 18th Fluid Dynamics and Plasmadynamics and Lasers Conference, Cincinnati, OH, July 1985, p. 7.

Weinberg, B.C., McDonald, H., Shamroth, S.J., “A Solution Procedure for Two and ThreeDimensional Unsteady Viscous Flows.” AIAA 23rd Aerospace Sciences Meeting, Reno, NV, Jan. 1985, p. 15.

Yang, R.J., Weinberg, B.C., Shamroth, S.J., McDonald, H., “Numerical Solutions of the NavierStokes Equations for Two and ThreeDimensional Turbine Cascades with Heat Transfer,” Published in General Motors Corp, Final Report, July 1985, p. 160.

Lui, N.S., Shamroth, S.J., McDonald, H., “Numerical Simulation of Unsteady ThreeDimensional Turbulent Structures in Boundary Layer Flow,” Published in Scientific Research Associates, Inc., Final Report, November 1984 – May 1985, p. 45.

Kim, Y.N., Buggeln, R.C., McDonald H., “Development of a NavierStokes Analysis for the Flow in Disk Pumps,” Published in Scientific Research Associates, Inc. Final Report, September 1984 – March 1985, p. 45.

Swafford, T.W., “TimeDependent Inverse Solution of ThreeDimensional Compressible, Turbulent Integral BoundaryLayer Equations in Nonorthogonal Curvilinear Coordinates,” Lecture Notes in Physics, Vol. 218, SpringerVerlag, 1985, pp. 541545.

Melnik, R. E., "The Computation of Viscid/Inviscid Interaction on Airfoils with Separated Flow," Third Symposium on the Numerical and Physical Aspects of Aerodynamic Flows, California State University, Long Beach, CA, 2124 January 1985.

Melnik, R. E., "Similarity Solutions for Plane and Radial Jets Using a ke Turbulence Model," Trans. ASMC Journal ed Fluids Engineering, Vol. 107, No. 1 March 12, 1985, (coauthor).

Melnik, R. E., "A Method for Design of Closed Airfoils for Arbitrary Supercritical Speed Distributions," AIAA paper No. 855023, AIAA 3rd Applied Aerodynamics Conference, 1416 October 1985, (coauthor).

Melnik, R. E., "An Improved Viscid/Inviscid Interaction Procedure for Transonic Flow Over Airfoils," NASA Contract Report 3805, October 1985, (coauthor).

Melnik, R. E., "Grumfoil: A Computer Code for the Viscous Transonic Flow Over Airfoils" NASA Contractor Report B806, October 1985, (coauthor).
1984 (back to top)

Whitfield, D. L. and Jameson, A., "Euler Equation Simulation of PropellerWing Interaction in Transonic Flow,"Journal of Aircraft, Vol. 21, No. 11, November 1984, pp. 835839.

Whitfield, D. L. and Janus, J. M., "ThreeDimensional Unsteady Euler Equations Solution Using Flux Vector Splitting," AIAA Paper No. 841552, June 1984.

Whitfield, D. L., Thomas, J. L., Jameson, A., and Schmidt, W., "Computation of Transonic ViscousInviscid Interacting Flow," in Numerical and Physical Aspects of Aerodynamic Flows II, T. Cebeci, Editor, SpringerVerlag, New York, 1984, pp. 285295.

Kreskovsky, J. P., Briley, W. R. and McDonald, H., "Investigation of Mixing in a Turbofan Exhaust Duct, Part I: Analysis and Computational Procedure," AIAA Journal, Vol. 22, No. 3, pp. 374382, 1984.

Briley, W. R. and McDonald, H., "Three Dimensional Viscous Flows with Large Secondary Velocity," J. Fluid Mechanics, Vol. 144, pp. 4777, 1984 (coauthor).

Shamroth, S. J., McDonald, H. and Briley, W. R., "Prediction of Cascade Flow Fields Using the Averaged Navier Stokes Equations," Journal of Engineering for Gas Turbines and Power, Vol. 106, pp.383390, 1984.

McDonald, H. and Briley, W. R., "A Survey of Some Recent Work on Interacted Boundary Layer Theory for Flow with Separation," Proceedings, Symposium on Numerical and Physical Aspects of Aerodynamic Flows (Univ. California, Long Beach), Springer Verlag, 1984.

Briley, W. R. and McDonald, H., "Three Dimensional Viscous Flows with Large Secondary Velocity," ASME Symposium on Computation of Internal Flows: Methods and Applications, New Orleans, LA, 1984.

Arabshahi, A., “Correlations for the Drag Coefficient of Blunt Circular Cylinders in Transonic Axial Flow,” Master’s Thesis, May 1984.

J. P. Kreskovsky, Briley, W.R. and McDonald, H, "Investigation of Mixing in a Turbofan Exhaust Duct, Part I: Analysis and Computational Procedure," AIAA Journal, 22(3): 374382, 1984.

S. J. Shamroth, McDonald, H. and Briley, W. R, "Prediction of Cascade Flow Fields Using the Averaged Navier Stokes Equations," Journal of Engineering for Gas Turbines and Power, 106: 383390, 1984.

Sabnis, J.S., Gibeling, H.J., McDonald, H., “Internal Fluid Mechanism of Solid Propellant Rocket Motors,"Proceedings of 21st JANNAF Combustion Meeting, (Oct 1984) Vol. 1 p.p. 195205.

Weinberg, B.C., Yang, R.J., Shamroth, S.J., McDonald, H., “Calculation of Two and ThreeDimensional Transonic Cascade Flow Field Using the NavierStokes Equations,” Published by NASA Lewis Research Center’s Turbine Engine Hot Section Technology Report, October 1984, p. 8.

Briley, W. R., Buggeln, R.C., McDonald, H., “Solution of the ThreeDimensional NavierStokes Equations for a Steady Laminar Horseshoe Vortex Flow,” Scientific Research Associates, Inc., Final Report, June 1982 – June 1984, p. 43.

Shamroth, S.J., McDonald, H., Weinberg, B.C., Roscoe, D.V., “Development of a NavierStokes Rotor and Stator Analysis,” Scientific Research Associates, Inc., Annual Report, June 1984, p. 39.
1983 (back to top)

Swafford, T. W. and Whitfield, D. L., "Numerical Solutions of ThreeDimensional TimeDependent Compressible Turbulent Integral BoundaryLayer Equations in General Curvilinear Coordinates," AIAA Paper No. 831674, July 1983.

Levy, R., Briley, W. R. and McDonald, H., "Viscous Primary/Secondary Flow Analysis for Use with Nonorthogonal Coordinates," AIAA Paper No. 830556 (21st Aerospace Sciences Meeting, Reno, NV), 1983.

Briley, W. R., McDonald, H. and Shamroth, S. J., "A Low Mach Number Euler Formulation and Application to Time Iterative LBI Schemes," AIAA Journal, Vol. 21, No. 10, pp. 14671469, 1983.

Schmidt, W., Jameson, A., and Whitfield, D., "FiniteVolume Solutions to the Euler Equations in Transonic Flow,"Journal of Aircraft, Vol. 20, No. 2, February 1983, pp. 127133.

Whitfield, D. L. and Jameson, A., "ThreeDimensional Euler Equation Simulation of PropellerWing Interaction in Transonic Flow," AIAA Paper No. 830236, January 1983.

Liu, N.S., Shamroth, S.J., McDonald, H., “Numerical Solution of the NavierStokes Equations for Compressible Turbulent Two/Three Dimensional Flows in the Terminal Shock Region of an Inlet/Diffuser.” AIAA Paper 831892,AIAA 6th Computational Fluid Dynamics Conference, Danvers, MA (Jul. 1983), pp. 6171. 45.

Levy, R., Briley, W.R. and McDonald, H., "Viscous Primary/Secondary Flow Analysis for Use with Nonorthogonal Coordinates," AIAA Paper No. 83 0556, 21st Aerospace Sciences Meeting, Reno, NV, 1983.

Shamroth, S.J., Yang, R.J., McDonald, H., “Further Development of a Transonic Cascade Snalysis," Scientific Research Associates, Inc., Final Report, August 1983, p. 49.

Gibeling, H.J., Briley, W.R., Kreskovsky, J.P., Shamroth, S.J., McDonald, H., “Computation of Discrete Slanted Hole Film Cooling Flow Using the NavierStokes Equations,” Scientific Research Associates, Inc., Final Report, September 1983, p. 63.

Lin, S.J., Kreskovsky, J.P., Briley, W.R., McDonald, H., “Further Development of a Method for Computing ThreeDimensional Subsonic Viscous Flows in Turbofan Lobe Mixers,” Scientific Research Associates, Inc., Final Report, November. 1983, p. 66.

Swafford, T.W., “ThreeDimensional, TimeDependent, Compressible, Turbulent, Integral BoundaryLayer Equations in General Curvilinear Coordinates and Their Numerical Solution,” AEDCTR8337, Arnold AFB, TN, September 1983.

Swafford, T.W., “Analytical Approximation of Two Dimensional Separated Turbulent Boundary Layer Velocity Profiles,” AIAA Journal, Vol. 21, No. 6, June 1983, pp. 923926.

Swafford, T.W., “ThreeDimensional, TimeDependent, Compressible, Turbulent, Integral BoundaryLayer Equations in General Curvilinear Coordinates and Their Numerical Solution,” PhD Dissertation, Mississippi State University, August 1983.
1982 (back to top)

Whitfield, D. L., Swafford, T. W., and Donegan, T. L., "An Inverse Integral Computational Method for Compressible Turbulent Boundary Layers," in Recent Contributions to Fluid Mechanics, W. Haase, Editor, SpringerVerlag, Berlin, 1982.

McDonald, H., Shamroth, S. J. and Briley, W. R., "Transonic Flows with Viscous Effects. Transonic, Shock, and Multidimensional Flows: Advances in Scientific Computing," Academic Press, Inc., 1982.

Shamroth, S. J., McDonald, H. and Briley, W. R., "Application of a Navier Stokes Analysis to Transonic Cascade Flow Fields," ASME Paper 82 GT 235, 1982.

Briley, W. R. and McDonald, H., "Computation of Turbulent Horseshoe Vortex Flow Past Swept and Unswept Leading Edges," SRA Report R82 920001 F, 1982.

Briley, W. R., Buggeln, R. C. and McDonald, H., "Computation of Laminar and Turbulent Flow in 90 Degree Square Duct and Pipe Bends Using the Navier Stokes Equations," SRA Report R82 920009 F, 1982.

McDonald, H. and Briley, W.R.: Some Observations on Numerical Solution of the Three Dimensional Navier Stokes Equations: Numerical and Physical Aspects of Aerodynamic Flows, Edited by T. Cebeci, Springer Verlag, New York, pp. 99120, 1982.

Shamroth, S.J., McDonald, H. and Briley, W.R., "Application of a Navier Stokes Analysis to Transonic Cascade Flow Fields," ASME Paper 82 GT 235, 1982.

Kreskovsky, J.P., Briley, W.R., McDonald, H., “Turbofan Forced MixerNozzle Internal Flowfield. Volume 3; A Computer Code for 3D Mixing in Axisymmetric Nozzles,” Published in Scientific Research Associates, Inc., Final Report, April 1982, Vol. 3, p. 129.
1981 (back to top)

Whitfield, D. L., Swafford, T. W., and Jacocks, J. L., "Calculation of Turbulent Boundary Layers with Separation and ViscousInviscid Interaction," AIAA Journal, Vol. 19, No. 10, October 1981, pp. 13151322.

Schmidt, W., Jameson, A., and Whitfield, D. L., "Finite Volume Solution for the Euler Equation for Transonic Flow over Airfoils and Wings Including Viscous Effects," AIAA Paper No. 811265, June 1981.

Whitfield, D. L., Jameson, A., and Schmidt, W., "ViscidInviscid Interaction on Airfoils Using Euler and Inverse BoundaryLayer Equations," Presented at the U.S.German Data Exchange Meeting at DFVLRAVA in Gottingen, Germany, April 1981.

Kreskovsky, J.P., Briley, W.R, McDonald, H., “Analysis and Computation of ThreeDimensional Flow in Strongly Curved Ducts.” ASME Winter Annual Meeting, Washington, D.C., November 1981, A8229001 1302; American Society of Mechanical Engineers, 1981, pp. 129140.

Briley, W.R., McDonald, H., “Computation of ThreeDimensional Horseshoe Vortex Flow Using the Navier Stokes Equations.” 7th International Conference on Numerical Methods in Fluid Dynamics, Stanford and Moffett Field, CA, June 1980. Published Berlin and New York, SpringerVerlag, 1981, pp. 9198.

Buggeln, R.C., Briley, W.R., McDonald, H., “Solution of the NavierStokes Equations for ThreeDimensional Turbulent Flow with Viscous Sublayer Resolution.” AIAA paper 811023, Proceedings of the AIAA 5th Computational Fluid Dynamics Conference, Palo Alto, CA, June 1981. Collection of Technical Papers, 1981, pp. 247256.

McDonald, H. and W. R. Briley, "Some Observations on Numerical Solution of the Three Dimensional Navier Stokes Equations," Proceedings, Symposium on Numerical and Physical Aspects of Aerodynamic Flows (Univ. California, Long Beach), Springer Verlag, 1981.

Levy, R., McDonald, H., Briley, W.R., Kreskovsky, J.P., “A ThreeDimensional Turbulent Compressible Subsonic Duct Flow Analysis for Use with Constructed Coordinate Systems,” Scientific Research Associates, Inc., Final Report, 1981, p. 40.

Kreskovsky, J.P., Briley, W.R., McDonald, H., “Prediction of Laminar and Turbulent Primary and Secondary Flows in Strongly Curved Ducts,” Scientific Research Associates, Inc., Final Report, February 1981, p. 59.

Gibeling, H.J., Kreskovsky, J.P., Briley, W.R., McDonald, H., “Computation of Discrete Hole Film Cooling Flow Using the NavierStokes Equations,” Published in Scientific Research Associates, Inc., Annual Report, April 1980 – March 1981, p. 28.
1980 (back to top)

Whitfield, D. L., Swafford, T. W., and Jacocks, J. L., "Calculation of Turbulent Boundary Layers with Separation, Reattachment, and ViscousInviscid Interaction," AIAA Paper No. 801439, July 1980.

Whitfield, J. D., Pate, S. R., Kimzey, W. F., and Whitfield, D. L., "The Role of Computers in Aerodynamic Testing,"Computers and Fluids, Vol. 8, No. 1, March 1980, pp. 7199.

Briley, W. R. and McDonald, H., "On the Structure and Use of Linearized Block Implicit and Related Schemes,"Journal of Computational Physics, Vol. 34, p. 54, 1980.

Briley, W. R. and McDonald, H., "Computation of Three Dimensional Horseshoe Vortex Flow Using the Navier Stokes Equations," Proceedings, 7th International Conference on Numerical Methods in Fluid Dynamics," (Stanford Univ.), Springer Verlag, New York, 1980, pp. 9198.

Levy, R., McDonald, H. and Briley, W. R., "A Three Dimensional Turbulent Compressible Subsonic Duct Flow Analysis for Use with Constructed Coordinate Systems," AIAA Paper No. 80 1398, AIAA 13th Fluid and Plasma Dynamics Conference (Snowmass, CO), 1980.

Buggeln, R. C., Briley, W. R. and McDonald, H., "Computation of Laminar and Turbulent Flow in Curved Ducts, Channels, and Pipes Using the Navier Stokes Equations," SRA Report R80 920006 F, 1980.

Kreskovsky, J. P., Briley, W. R. and McDonald, H., "Computation of Discrete Hole Film Cooling Flow Using the Navier Stokes Equations," SRA Report R80 910002 2, 1980.

Shamroth, S.J., Gibeling, H.J., McDonald, H., “A NavierStokes solution for laminar and turbulent flow through a cascade of airfoils.” Proceedings of the AIAA 13th Fluid and Plasma Dynamics Conference, Snowmass, CO, (Jul. 1980), p. 14.

Buggeln, R.C., McDonald, H., Kreskovsky, J.P., Levy, R., “Computation of ThreeDimensional Viscous Supersonic Flow in Inlets.” AIAA Paper 800194, AIAA 18th Aerospace Sciences Meeting, Pasadena, CA, January 1980, p. 12.

Buggeln, R.C., McDonald, H., Levy, R., Kreskovsky, J.P., “Development of a ThreeDimensional Supersonic Inlet Flow Analysis,” Scientific Research Associates, Inc., Final Report, January 1980, p. 122.

Swafford, T.W., “Analytical Approximation of Two Dimensional Separated Turbulent Boundary Layer Velocity Profiles,” AEDCTR7999, Arnold AFB, TN, October 1980.

Swafford, T.W., “Computational Support to Tests at AEDC/PWT,” AEDCTMR80P32, Arnold AFB, TN, September 1980 (Limited Distribution).
1979 (back to top)

Whitfield, D. L., "Analytical Description of the Complete Turbulent Boundary Layer Velocity Profile," AIAA Journal, Vol. 17, No. 10, October 1979, pp. 11451147.

Briley, W. R. and McDonald, H., "Analysis and Computation of Viscous Subsonic Primary and Secondary Flows," AIAA 4th Computational Fluid Dynamics Conference (Williamsburg, VA), 1979.

McDonald, H. and Briley, W. R., "Computational Fluid Dynamic Aspects of Internal Flows," Invited Paper, AIAA 4th Computational Fluid Dynamics Conference (Williamsburg, VA), 1979, pp. 266 283.

Shamroth, S. J. and Briley, W. R., "A Viscous Flow Analysis of the Tip Vortex Generation Process," AIAA Paper No. 79 1546, 12th Fluid and Plasma Dynamics Conference (Williamsburg, VA) 1979.

McDonald, H., “Combustion modeling in two and three dimensions – Some numerical considerations.” Progress in Energy and Combustion Science, Vol 5, No. 2, (1979) pp. 97122.

Levy, R., Briley, W.R., McDonald, H., “Viscous Flow in the Region of a Rounded Trailing Edge,” Scientific Research Associates, Inc., Final Report, July 1978 – June 1979, p. 41.

McDonald H., “Computational Aspects of Viscous Flows (Numerical Analysis of Viscous Flow and the Relationship of the Boundary Layer Equations to the NavierStokes Equation,” Scientific Research Associates, Inc., Published in Von Karman Institute for Fluid Dynamics Application of Numerical Methods to Flow Calculations in Turbomachines, 1979, p. 192.

Kreskovsky, J.P., Briley, W.R., McDonald, H., “Computation of Discrete Hole Film Cooling Flow Using the NavierStokes Equations (Gas Turbine Blades),” Scientific Research Associates, Inc., Final Report, July 1979, p. 17.

Weinberg, B.C., McDonald, H., “Solution of 3Dimensional TimeDependent Viscous Flows. Part 1: Investigation of Candidate Algorithms (1979); Part 2: Development of Computer Code (1980); Part 3: Application to Turbulent and Unsteady Flows (1982), ” Scientific Research Associates, Inc. Report Number NASACR166565PT1, April 1979, p. 86.

Swafford, T.W., Calculation of Skin Friction in Two Dimensional, Transonic, Turbulent Flow,” AEDCTR7912, Arnold AFB, TN, 1979.
1978 (back to top)

Whitfield, D. L., "Integral Solution of Compressible Turbulent Boundary Layers Using Improved Velocity Profiles," AEDCTR7842, August 1978.

Sinclair, D. W., Whitfield, D. L., and Lucci, C. A., "Holographic Interferometry Measurements of Subsonic Turbulent Boundary Layers," AIAA Paper No. 78119, July 1978.

McDonald, H. and Briley, W. R., "A Review of Computational Methods for the Compressible Navier Stokes Equations in Turbomachinery Applications," SRA Report 78 2, Detroit Diesel Allison, April 1978.

Whitfield, D. L., "Analytical Description of the Complete Turbulent Boundary Layer Velocity Profile," AIAA Paper No. 781158, 1978.

Levy R., McDonald, H., Briley, W.R., “Calculation of ThreeDimensional Turbulent Subsonic Flow in Transition Ducts,” Proceedings of 6th International Conference on Numerical Methods in Fluid Dynamics, Tiflis, GA, June 1978, pp. 361369.

Eiseman, P.R., Levy, R., McDonald, H., Briley, W.R., “Development of a ThreeDimensional Turbulent Duct Flow Analysis,” United Technologies Research Center, East Hartford, CT., Final Report, November 1978, p. 117.

Anderson, O. L., Briley, W.R., McDonald H., “Derivation and Evaluation of an Approximate Analysis for ThreeDimensional Viscous Subsonic Flow with Large Secondary Velocities (Finite Difference Method),” United Technologies Research Center, East Hartford, CT, Final Report, October 1978, p. 84.
1977 (back to top)

Whitfield, D. L., "Analytical Description of the Complete TwoDimensional Turbulent BoundaryLayer Velocity Profile," AEDCTR7779, September 1977.

Whitfield, D. L., "Turbulent Flow Near a Wall Based on a Turbulent Kinetic Energy Equation," in Boundary Layer EffectsProceedings of the 5th U.S. Air ForceFederal Republic of Germany Data Exchange Agreement Meeting, A.W. Fiore, Editor, AFFDLTR7761, July 1977, pp. 447454.

Whitfield, D. L. and High, M. D., "VelocityTemperature Relations in Turbulent Boundary Layers with NonUnity Prandtl Numbers," AIAA Journal, Vol. 15, No. 3, March 1977, pp. 431434.

Briley, W. R. and McDonald, H., "Solution of the Multidimensional Compressible Navier Stokes Equations by a Generalized Implicit Method," Journal of Computational Physics, Vol. 24, No. 4, 1977, pp. 372397.

Kreskovsky, J. P., Shamroth, S. J. and Briley, W.R., "A Numerical Study of the Unsteady Leading Edge Separation Bubble on an Oscillating Airfoil," Computer Methods in Applied Mechanics and Engineering, Vol. 11, pp. 39 56, 1977.

Eiseman, P.R., Levy, R., McDonald, H., “A Method for Computing Flows Over an Ogival Body,” United Technologies Research Center, East Hartford, CT. Final Report, July1977, p. 51.
1976 (back to top)

Whitfield, D. L., "Analytical, Numerical and Experimental Results on Turbulent Boundary Layers," AEDCTR7662, July 1976.

Whitfield, D. L. and High, M. D., "VelocityTemperature Relations in Turbulent Boundary Layers with NonUnity Prandtl Numbers," AIAA Paper No. 76411, July 1976.

Whitfield, D. L., "Infrared Turbojet Plume Radiation," AEDCTR7614, February 1976.

Hall, G.F., Shamroth, S.J., McDonald, H., Briley, W.R., “The Inviscid Pressure Field on the Tip of a SemiInfinite Wing and Its Application to the Formation of a Tip Vortex,” United Technologies Research Center, East Hartford, CT, Final Report, October 1976, p. 84.

Gibeling, H.J., McDonald, H., “Development of a ThreeDimensional Combustor Flow Analysis. Volume 2: Theoretical Studies,” United Technologies Research Center, East Hartford, CT., Final Report, June 1975 – October 1976, p. 61.

Levy, R., Shamroth, S.J., Gibeling, H.J., McDonald, H., “A Study of the Turbulent Shock Wave Boundary Layer Interaction.” United Technologies Research Center, East Hartford, CT., Final Report, July 1973 – October 1976, p. 80.

Swafford, T.W., “An Experimental and Analytical Investigation of a Radial Face Seal,” MS Thesis, University of Tennessee, Knoxville, TN, 1976.
1975 (back to top)

Whitfield, D. L., Bertrand, W. T., and Brewer, L. E., "Infrared Radiation Approximation for Homogeneous Plumes," AIAA Paper No. 75703, May 1975.

McDonald, H. and Briley, W. R., "Three Dimensional Supersonic Flow of a Viscous or Inviscid Gas," Journal of Computational Physics, Vol. 19, No. 2, 1975, pp. 150178.

Briley, W. R. and McDonald, H., "Numerical Prediction of Incompressible Separation Bubbles," Journal of Fluid Mechanics, Vol. 69, Part 4, 1975, pp. 631656.

Gibeling, H. J., Briley, W. R. and McDonald, H., "Development of a Three Dimensional Combustor Flow Analysis,"Vol. I: Theoretical Studies. AFAPL TR 75 59, 1975.

Shamroth, S.J., McDonald, H., “Application of a Transitional BoundaryLayer in the Low Hypersonic Mach Number Regime,” International Journal of Heat and Mass Transfer, Vol. 18, Nov. 1975, pp. 12771284.

Kreskovsky, J.P., Shamroth, S.J., McDonald, H., “Application of a General Boundary Layer Analysis to Turbulent Boundary Layers Subjected to Strong Favorable Pressure Gradients.” ASME paper 75FE16, ASME, Joint Fluids Engineering and Lubrication Conference, Minneapolis, MN, May, 1975, p. 12.

Briley, W. R., McDonald, H., Gibeling, H.J., “Solution of the Multidimensional Compressible NavierStokes Equations by a Generalized Implicit Method,” United Technologies Research Center, East Hartford, CT, Final Report, March 1972 – December 1975, p. 63.
1974 (back to top)

Whitfield, D. L., "Some Computations of Turbulent Boundary Layers," ARO ER743, August 1974.

Whitfield, D. L., "Some Improvements in Data Reduction of Pitot Pressure Measurements in Turbulent Boundary Layers," AROER744, August 1974.

Whitfield, D. L., Lewis, J. W. L., and Williams, W. D., "Measurements in the Near Field of Supersonic Nozzles for Chemical Laser Systems," AIAA Journal, Vol. 12, No. 6, June 1974, pp. 870872.

Whitfield, D. L., "Heat Flux to Normal Flat Plates in Rarefied Hypersonic Flow," Rarefied Gas Dynamics, Vol. II, DFVLRPress, PorzWahn, German, 1974, pp. D.18.1D.18.7.

Briley, W.R., "A Numerical Method for Predicting Three Dimensional Viscous Flows in Ducts," Journal of Computational Physics, Vol. 14, No. 1, 1974, pp. 828.

Briley, W. R. and McDonald, H., "Solution of the Three Dimensional Compressible Navier Stokes Equations by an Implicit Technique," Proceedings, 4th International Conference on Numerical Methods in Fluid Dynamics, Univ. Colorado, Boulder CO, Springer Verlag, New York, 1974, pp. 105 110.

McDonald, H., Kreskovsky, J.P., “Effect of free stream turbulence on the turbulent boundary layer,” International Journal of Head and Mass Transfer, Vol. 17, July 1974, pp. 705716.

Kreskovsky, J.P., Shamroth, S.J., McDonald, H., “Parametric Study of Relaminarization of Turbulent Boundary Layers on Nozzle Walls,” United Technologies Research Center, East Hartford, CT., Final Report, June 1974, p. 93.

Anasoulis, R.F., McDonald, H., Buggeln, R.C., “Development of a Combustor Flow Analysis. Part 1: Theoretical Studies,” United Technologies Research Center, East Hartford, CT., Final Report, April 1974, p. 91.
1973 (back to top)

Whitfield, D. L., "Mean Free Path of Emitted Molecules and Correlation of Sphere Drag Data," AIAA Journal, Vol. 11, No. 12, December 1973, pp. 16661670.

Whitfield, D. L., Smithson, H. K., and Price, L. L., "Plume Boundary Jump of an Underexpanded Jet Exhausting Counter to a Freestream," AIAA Journal, Vol. 11, No. 9, September 1973, pp. 13361337.

Whitfield, D. L., Lewis, J. W. L., and Williams, W. D., "Specie Number Density, Pitot Pressure, and Flow Visualization in the Near Field of Two Supersonic Nozzle Banks Used for Chemical Laser Systems," AIAA Paper No. 73642, July 1973.

Whitfield, D. L., "Viscous Effects in LowDensity Nozzle Flows," AEDCTR7352, June 1973.

Whitfield, D. L., Lewis, J. W. L., Williams, W. D., et al., "Specie Number Density, Pitot Pressure, and Flow Visualization in the Near Field of Two Supersonic Nozzle Banks Used for Chemical Laser Systems," AEDCTR7311, May 1973.

Whitfield, D. L., "Calibration of a Heat Flux Sensor in Rarefied Hypersonic Flow," LTRAEDCVKFASP373, March 1973.

Whitfield, D. L., "Rarefied Flow HeatFlux Calibration of an Earth Satellite Temperature Alarm System," LTRAEDCVKFASP173, March 1973.

Briley, W. R., "The Computation of Three Dimensional Viscous Internal Flows," Proceedings, 3rd International Conference on Numerical Methods in Fluid Dynamics (Paris, France), Vol. II, Springer Verlag, New York, 1973, pp. 33 38.

Whitfield, D. L., "Mean Free Path of Molecules from a Surface in Rarefied Flow with Application to Correlating Drag Data," AIAA Paper No. 73198, January 1973.

McDonald, H., Fish, R.W., “Practical Calculations of Transitional Boundary Layers,” International Journal of Heat and Mass Transfer, Vol. 16, Sept. 1973, pp. 17291744.

Anasoulis, R.F., McDonald, H., “A Study of Combustor Flow Computations and Comparison With Experiment.” United Technologies Research Center, East Hartford, CT., Final Report, December 1973, p. 97.

Anasoulis, R.F., McDonald, H., “Development of a Combustor Flow Analysis. Part 2; Experimental Studies,” United Technologies Research Center, East Hartford, CT. Final Report, June– September 1973, p. 38.

Briley, W.R., McDonald, H., “An Implicit Numerical Method for the Multidimensional Compressible NavierStokes Equations (Application to Three Dimensional Subsonic Flow),” United Technologies Research Center, East Hartford, CT. Report, November 1973, p. 56.
1972 (back to top)

Shamroth, S.J., McDonald, H., “Application of a TimeIndependent BoundaryLayer Analysis to the Problem of Dynamic Stall.” ASME, Transactions Journal of Applied Mechanics, Vol. 39, Sept. 1972, pp. 823825.

Shamroth, S.J., McDonald, H., “A New Solution of the Turbulent NearWake Recompression Problem. (CroccoLee Theory Extension to Flow Behavior Prediction for Two Dimensional Supersonic Turbulent Near Wake Behind Bluff Body During Recompression).” Aeronautical Quarterly, Vol. 23, May 1972, pp. 121130.

McDonald, H., Fish, R. W., “Practical Calculations of Transitional Boundary Layers (Finite Difference Procedure for Computing Behavior of TwoDimensional Boundary Layers and Turbulence Model to Predict Location and Extent of Transition Region,” Published in AGARD Boundary Layer Effects in Turbomachines, December 1972, pp. 2953.

Shamroth, S.J., McDonald H., “Assessment of a Transitional Boundary Layer Theory at Low Hypersonic Mach Numbers (Accuracy of Transitional Boundary Layer Theory in Low Hypersonic Mach Number Range),” United Technologies Research Center, East Hartford, CT. Report, November 1972, p. 69.
1971 (back to top)

Whitfield, D. L., "Drag on Bodies in Rarefied HighSpeed Flow," PhD Dissertation, University of Tennessee, December 1971.

Stephenson, W. B. and Whitfield, D. L., "Drag Measurement in a Low Density Gas Stream," IEEE Transactions on Aerospace Electronic Systems, Vol. 7, No. 6, November 1971, pp. 11311137.

Powell, H. M., Hill, D. W., and Whitfield, D. L., "Evaluation of a Mass Spectrometer Probe for Density and Velocity Distribution Measurements in a Rocket Exhaust Plume," AEDCTR71135, September 1971.

Smithson, H. K., Price, L. L., and Whitfield, D. L., "Wind Tunnel Testing of Interactions of High Altitude Rocket Plumes with the Free Stream," AEDCTR71118, September 1971.

Whitfield, D. L. and Smithson, H .K., "LowDensity Supersonic Sphere Drag with Variable Wall Temperature," AEDCTR7183, July 1971.

Powell, H. M., Hill, D. W., and Whitfield, D. L., "The Measurements and Analysis of Chemical and Gas Dynamic Properties of a Rocket Plume at Near Space Conditions (U)," JANNAF Sixth Plume Technology Meeting, Naval Postgraduate School, Monterey, CA, 1971, CPIA Publication 209, April 1971. (CONFIDENTIAL)

Whitfield, D. L., "Analysis of Sphere and Cylinder Drag in Rarefied Flow," Rarefied Gas Dynamics, Vol. I., Editrice Tecnico Scientifica, Pisa, Italy, 1971, pp. 527534.

Briley, W. R., "A Numerical Study of Laminar Separation Bubbles Using the Navier Stokes Equations," Journal of Fluid Mechanics, Vol. 47, Part 4, pp. 713736, 1971.

Briley, W. R., "An Analysis of Laminar Separation Bubble Flow Using the Navier Stokes Equations," Invited paper,Specialists Workshop on Unsteady, Three Dimensional and Separated Flow (Georgia Tech. Univ.), 1971. (Proceedings published by Purdue Univ.).

Briley, W. R. and Walls, H. A., "Numerical Study of Time Dependent Rotating Flow in a Cylindrical Container at Low and Moderate Reynolds Numbers," Proceedings, 2nd International Conference on Numerical Methods in Fluid Dynamics (Univ. California, Berkeley), Springer Verlag, New York, 1971, pp. 377384.

Stephenson, W. B. and Whitfield, D. L., "Drag Measurement in a Low Density Gas Stream," IEEE Transactions on Aerospace Electronic Systems, Vol. 7, No. 6, November 1971, pp. 11311137.

McDonald, H., Shamroth, S.J., “An Analysis and Application of the TimeDependent Turbulent BoundaryLayer Equations (Two Dimensional Compressible Turbulent Boundary Layer with Time Dependent Mean Velocity and Density Fields, Deriving Momentum and Kinetic Energy Integral Equations),” AIAA Journal, Vol. 9, Aug. 1971, pp. 15531560.
1970 (back to top)

Benek, J. A. and Whitfield, D. L., "AFRPL Scarfed Nozzle Condensation Study in 4x6 Research Chamber," LTRAEDCVKFASP170, December 1970.

Whitfield, D. L., "Dynamics of Particles in Free Molecular Flow with Application to High Altitude Meteoric Dust Collection Devices," AEDCTR70139, August 1970.

Whitfield, D. L. and Lewis, C. H., "BoundaryLayer Analysis of LowDensity Nozzles Including Displacement, Slip, and Transverse Curvature," Journal of Spacecraft and Rockets, Vol. 7, No. 4, April 1970, pp. 462468.

Whitfield, D. L. and Stephenson, W. B., "Sphere Drag in the FreeMolecular and Transitional Flow Regimes," AEDCTR7032, April 1970.

Stephenson, W. B. and Whitfield, D. L., "Drag Measurements in a Low Density Gas Stream," AEDCTR7025, May 1970.

McDonald, H., “A New Solution of the Turbulent NearWake Recompression Problem (Two Dimensional Supersonic Turbulent Near Wake Saddle Point Singularity During Recompression Analyzed by Including Transverse Momentum Integral Equation,” AIAA Paper 70228, AIAA 8th Aerospace Sciences Meeting, New York, N.Y., January 1970, p. 12.
1969 (back to top)

Whitfield, D. L. and Tidwell, E. D., "Low Density Wind Tunnel Measurements of the Chemiluminescent Reactions of Nitric Oxide with Atomic Oxygen and Atomic Hydrogen," AEDCTR69196, November 1969.

Whitfield, D. L. and Lewis, C. H., "Analysis of Boundary Layers in Low Density Hypersonic Axisymmetric Nozzles, Including the Effects of Displacement, FirstOrder Transverse Curvature, Velocity Slip, and Temperature Jump," AIAA Paper No. 69653, June 1969.

Good, R. E., Golmb, D., DelGreco, F. P., Hill, D. W., and Whitfield, D. L., "Clusters in Nitric Oxide Jet Expansion,"Rarefied Gas Dynamics, Vol. I., New York: Academic Press, 1969, pp. 14491453.

McDonald H., “Linear Stress Distribution and the Turbulent BoundaryLayer Equations of Motion,” Physics of Fluids, Vol. 12, Nov. 1969, pp. 22412247.

McDonald, H., “The Effect of Pressure Gradient on the Law of the Wall in Turbulent Flow,” Journal of Fluid Mechanics, Vol. 35, February 1969, pp. 311336.
1968 (back to top)

Whitfield, D. L., "Theoretical and Experimental Investigation of Boundary Layers in Low Density Hypersonic Axisymmetric Nozzles," AEDCTR68193, September 1968. (Also MS Thesis, University of Tennessee, June 1968.)

Briley, W.R., "Time Dependent Rotating Flow in a Cylindrical Container," PhD Dissertation, The University of Texas at Austin, August 1968.

McDonald, H., “The Departure from Equilibrium of Turbulent Boundary Layers,” Aeronautical Quarterly, Vol. 19, Feb. 1968, pp. 119.

Maise, G., McDonald, H., “Mixing Length and Kinematic Eddy Viscosity in a Compressible Boundary Layer,” AIAA Journal, Vol. 6, Jan. 1968, pp. 7380.

Camarata, F.J., McDonald, H., “An Extended Mixing Length Method for Computing Turbulent Shear Stress Distribution Required in Calculating Two Dimensional Incompressible Turbulent Boundary Layer,” Stanford University, Department of Mechanical Engineering, Thermosciences Div., 1969, p. 16; and Volume 1 – Methods, Predictions, Evaluation and Flow Structures, August 1968, pp. 8398.
1967 (back to top)

Briley, W. R., "Reynolds Number Effect on Transient Behavior of Swirling Flow in a Cylindrical Vessel," M. S. Thesis, The University of Texas at Austin, January 1967.
1964 (back to top)

McDonald, H., “Turbulent Shear Layer Reattachment With Special Emphasis on the Base Pressure Problem,”Aeronautical Quarterly, Vol. 15, Aug. 1964, pp. 247280.