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 2014 (back to top)

  1. Mittal, A., Sreenivas, K., and Taylor, L.K., "Exploration of Modal Decomposition Techniques for Wind Turbines," AIAA-2014-1398, SciTech 2014, National Harbor, MD, January 2014.
  2. Karman, S. L., "Multi-Block Hierarchical Unstructured Grid Generation With Adaptation," AIAA-2014-0116, SciTech 2014, National Harbor, MD, January 2014.

2013 (back to top)

  1. Ahrabi, B.R., Sreenivas. K., and Webster, R.S., "Computational Investigation of Compressible Flow in a Diffusing S-duct," 49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference. San Jose, CA, July 2013, AIAA Paper 2013-3601.
  2. 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 2013-3621.
  3. 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 2013-3632.
  4. Sreenivas, K, Hilbert, C.B., Mittal, A., Hereth, L., and Taylor, L.K., "High-Fidelity Computational Simulation of the Wake Characteristics of a Model Wind Turbine," 31st AIAA Applied Aerodynamics Conference, San Diego, CA, June 2013, AIAA Paper 2013-2416.
  5. Erwin, T., Anderson, W.K., Kapadia, S. and Wang, L., “Three Dimensional Stabilized Finite Elements for Compressible Navier-Stokes”, AIAA Journal, 51(6), pp. 1404-1419, 2013.
  6. Anderson, W.K., Wang, L., Newman, J. and Kapadia, S., “Extension of the Petrov Galerkin Time-Domain Algorithm for Dispersive Media”, IEEE Microwave And Components Letters, 23(5), pp. 234-236, 2013.
  7. Erwin, T., Anderson, W.K., Wang, L., and Kapadia, S., “High-order Methods for Solutions of Three-dimensional Turbulent Navier-Stokes”, AIAA 2013-2571, 21st AIAA Computational Fluid Dynamics Conference, June 2013.
  8. Briley, W. Roger, "An Introduction to Vectors and Tensors from a Computational Perspective," Report UTC-CECS-SimCenter-2013-01, May 3013.
  9. 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 2013-2894.
  10. Glasby, R., Burgess, N., Anderson, W.K., Wang, L., Allmaras, S. and Mavriplis, D., "Comparison of SU/PG and DG Finite-Element Techniques for the Compressible Naiver-Stokes Equations on Anisotropic Unstructured Meshes," AIAA paper 2013-0691, 51st AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, Dallas, TX, 07-10 January, 2013.
  11. O'Connell, M. and Karman Jr., S. L., "Mesh Rupturing: A Technique for Geometry Insertion and Significant Mesh Movement," AIAA Paper 2013-1048, 51st AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, Dallas, TX, 07-10 January, 2013.
  12. Wang, L., Anderson, W.K, Erwin, T., and Kapadia, S., "High-order Methods for Solutions of Three-dimensional Turbulent Flows," AIAA Paper 2013-0856, 51st AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, Dallas, TX, 07-10 January, 2013.

2012 (back to top)

  1. 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 9-15, 2012.
  2. Webster, R., Whitfield, D., Hilbert, B., Sreenivas, K., Hyams, D. and Briley, W., "Demonstration of Sub-system Level Simulations: A Coupled Inlet and Turbofan Stage," AIAA Paper 2012-4282, 48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Atlanta, GA, 2012.
  3. 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. 2080-2090, October 2012.
  4. Wang, Li and Anderson, W. Kyle, “Shape Sensitivity Analysis for the Compressible Navier-Stokes Equations Via Discontinuous Galerkin Methods”, Computers & Fluids, Vol. 69, pp. 93-107, 2012.
  5. Ghasemi, A., Sreenivas, K., and Taylor, L.K., "Unconditionally stable high-order picard iteration algorithm for computational electromagnetics," IEEE Antennas and Propagation Society International Symposium (APSURSI), 8 - 14 July 2012 , Chicago, IL.
  6. Wang, Li, Anderson, W. Kyle, Erwin, Taylor, and Kapadia, Sagar, “Solutions of High-order Methods for Three-dimensional Compressible Viscous Flows”, AIAA Paper 2012-2836, the 42nd AIAA Fluid Dynamics Conference, New Orleans, LA, June 2012.
  7. Druyor Jr., C., Karman, S. "An Adaptive Hybrid Grid Generation Method for Complex Geometries", AIAA-2012-157, 50th AIAA Aerospace Sciences Meeting, Nashville, TN, January 2012.
  8. O'Connell, M., Karman, S. "Techniques for Unstructured Mesh Adaptation with Elliptic Smoothing", AIAA-2012-156, 50th AIAA Aerospace Sciences Meeting, Nashville, TN, January 2012.
  9. 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 2012-0475, 50th AIAA Aerospace Sciences Meeting, 9 - 12 January 2012, Nashville, TN.
  10. Brock, W., Burdyshaw, C., Karman, S., Betro, V., Hilbert, B., Anderson, K., Haimes, R., "Adjoint-Based Design Optimization Using CAD Parameterization Through CAPRI", AIAA-2012-968, 50th AIAA Aerospace Sciences Meeting, Nashville, TN, January 2012.

2011 (back to top)

  1. 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 11-17, 2011.
  2. Ghasemi, A., and Sreenivas, K., “On the Theory of a Novel High-Order Time-Marching Algorithm Based on Picard Iteration,” UTC-CECS-SimCenter-2011-02, September 2011.
  3. Anderson, W. Kyle, Wang, Li, Kapadia, Sagar, Tanis, Craig, and Hilbert, Bruce, “Petrov-Galerkin and discontinuous Galerkin methods for time-domain and frequency-domain electromagnetic simulations,” J. of Comp. Physics, Vol. 230, pp. 8360-8385, 2011. DOI: 10.1016/j.jcp.2011.06.025, Available online Sept. 15, 2011.
  4. Arabshahi, A., Taylor, L.K., and Whitfield, D.L. “Computation of Dynamic Stability and Control Derivatives,” AIAA-2011-3348, 29th AIAA Applied Aerodynamic Conference, Honolulu, Hawaii, June 27-30, 2011.
  5. Wang, L. and Anderson, W.K., “Adjoint-Based Shape Optimization for Electromagnetic Problems Using Discontinuous Galerkin Method,” AIAA Journal, Vol. 49, No. 6, pp 1302-1305, 2011.
  6. Wang, L. and Anderson, W.K., “Sensitivity Analysis for the Compressible Navier-Stokes Equations Using A Discontinuous Galerkin Method,” AIAA-2011-3408, 41st AIAA Fluid Dynamics Conference, June, 2011, Honolulu, Hawaii.  
  7. Hyams, D., Sreenivas, K., Webster, R., Currier, N., “A Generalized, Unstructured Interpolative Interface method for Rotor-Stator Interactions,” AIAA-2011-3700, 20th AIAA Computational Fluid Dynamics Conference, Honolulu, Hawaii, June 27-30, 2011.
  8. Erwin, J. Taylor, Anderson, W. Kyle, Wang, Li, and Kapadia, Sagar, “Three Dimensional Stabilized Finite Elements for Compressible Navier-Stokes,” 41st AIAA Fluid Dynamics Conference, June, 2011, Honolulu, Hawaii.
  9. Nichols, III, D. S., “Accounting for Shocks in Turbulence Modeling,” 41st AIAA Fluid Dynamics Conference, June, 2011, Honolulu, Hawaii.
  10. Epstein, J.M., Pankajakshan, R., Hammond, R.A., “Combining Computational Fluid Dynamics and Agent-Based Modeling: A New Approach to Evacuation Planning,” PLoS ONE: Research Article, published 31 May 2011 10.1371/journal.pone.0020139.
  11. 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.
  12. Briley, W. R. and McDonald, H., “Reflections on the Evolution of Implicit Navier–Stokes Algorithms,” Computers & Fluids, 41:15-19, 2011.
  13. Pankajakshan, R., Mitchell, B.J., and Taylor, L.K., “Simulation of unsteady two-phase flows using a parallel Eulerian-Lagrangian approach,” Computers & Fluids, Volume 41, Issue 1, February 2011, Pages 20-26.
  14. 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 27-40.
  15. Karman, Jr., S.L., “Virtual Control Volumes for Three-Dimensional Unstructured Elliptic Smoothing,” AIAA-2011-893, 49th AIAA Aerospace Science Meeting, Orlando FL, January 2011.
  16. Betro, V. and Karman, Jr., S.L., “Fully Anisotropic Split-Tree Adaptive Refinement Mesh Generation Using Tetrahedral Mesh Stitching,” Proceedings of the 49th Annual AIAA Aerospace Sciences Meeting, Orlando, FL, January 4-7, 2011. AIAA-2011-0895.
  17. 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, 41-50.

2010 (back to top)

  1. 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.
  2. 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.
  3. Betro, V., “Implementing a Node-Based Split-Tree Neighbor Search Algorithm,” Research Note, 19th Annual International Meshing Roundtable, Chattanooga, TN, October 6-8, 2010.
  4. Karman, S.L. Jr., “Virtual Control Volumes for Two-Dimensional Unstructured Elliptic Smoothing,” 19th International Meshing Roundtable, paper 2A.4, Chattanooga, TN, October, 2010.
  5. Hyams, Daniel G., Kress, Reid, and Swafford, Tim W., “CFD‐Driven Agent‐Based Dispersion Modeling of the Y‐12 National Security Complex,” UTC-CECS-SimCenter-2010-01-R, September 2010.
  6. 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, 12-17 Sep. 2010.
  7. Betro, V. C., “Fully Anisotropic Split-Tree Adaptive Refinement Mesh Generation Using Tetrahedral Mesh Stitching,” PhD Dissertation, University of Tennessee at Chattanooga, August 2010.
  8. 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 28-1, 2010. Paper No. 2010-5097.
  9. 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 14-18, 2010. Paper GT2010-23414.
  10. Ji, L., Wilson, R., Sreenivas, K., and Hyams, D., “A Parallel Universal Mesh Deformation Scheme,” 28th AIAA Applied Aerodynamics Conference, June 2010, Chicago, AIAA-2010-4938.
  11. 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 14-16, 2010, Brooklyn, New York.
  12. Wang, Li, Mavriplis, Dimitri J. and Anderson, W. Kyle, “Unsteady Discrete Adjoint Formulation for High-order Discontinuous Galerkin Discretizations in Time-dependent Flow Problems,” 48th AIAA Aerospace Science Meeting, January 2010, Orlando, FL, AIAA-2010-367.
  13. Johnson, B. C., Webster, R. S., and Sreenivas K. “A Numerical Investigation of S-Duct Flows with Boundary-Layer Ingestion,” 48th AIAA Aerospace Science Meeting, January 4th-January 7th, 2010, Orlando, Florida, AIAA-2010-841.
  14. Webster, R., Hyams, D., Sreenivas, K., “Unstructured Grid Technology Applied to Axial-flow Compressors,” AIAA-2010-1605, 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, Orlando, Florida, Jan. 4-7, 2010.  

2009 (back to top)

  1. Li Wang and Dimitri J. Mavriplis, “Adjoint-based h-p Adaptive Discontinuous Galerkin Methods for the 2D Compressible Euler Equations,” Journal of Computational Physics, Vol. 228, Issue 20, pp 7643-7661, November 2009.
  2. 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 DE-FG02-05ER64076, September 2009.
  3. Karman, Jr., S.L., Mitchell, B., Sawyer, S., and Whitt, J., “Numerical Solutions for the CAWAPI Configuration on Unstructured Grids at UT-SimCenter, United States,” in Understanding and Modeling Vortical Flows to Improve the Technology Readiness Level for Military Aircraft, NATO RTO-TR-AVT-113, pp.14-1-36, RTO/NATO, 2009.
  4. Sivakumar, P., Hyams, D.G., Taylor, L.K., and Briley, W.R., “A Primitive-Variable Riemann Method for Solution of the Shallow-Water Equations with Wetting and Drying,” Journal of Computational Physics, Vol. 228, No.19, pp. 7452-7472, 2009.
  5. Arabshahi, A., Webster, R., Sreenivas, K., Hyams, D.G., and Whitfield, D.L., “Numerical Simulation of Reacting and Non-Reacting Nozzle Flows,” AIAA-2009-4858, 45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Denver Colorado, August 2009.
  6. Sreenivas, K., Taylor, Lafayette K., Briley, W. Roger, “Unsteady Flow Simulations for an Aerotonomy-Designed Synthetic-Jet Airfoil,” UTC-CECS-SimCenter-2009-02-R, June 2009.
  7. Kapadia, S., Anderson, W. K., and Burdyshaw, C., “Channel Shape Design of Solid Oxide Fuel Cells,” UTC-CECS-SimCenter-2009-01, June 2009.
  8. Karman, S., et al., "CFD Modeling of F-35 Using Hybrid Unstructured Meshes," AIAA Paper 2009-3662, 19th AIAA CFD Conference, San Antonio, TX, June 22-25 2009
  9. Dweik, Z., Briley, W.R., Swafford, T.W., and Hunt, B., “Computational Study of the Heat Transfer of the Buoyancy-Driven Rotating Cavity with Axial Throughflow of Cooling Air,” GT2009-59978, ASME Turbo EXPO 2009, June 8-12, 2009, Orlando, FL.
  10. Dweik, Z., Briley, W.R., Swafford, T.W., and Hunt, B., “Computational Study of the Unsteady Flow Structure of the Buoyancy-Driven Rotating Cavity with Axial Throughflow of Cooling Air,” GT2009-59969, ASME Turbo EXPO 2009, June 8-12, 2009, Orlando, FL.
  11. Anderson, W.K., Karman, S.L., and Burdyshaw, C., “Geometry Parameterization Method for Multidisciplinary Applications,” AIAA Journal, Vol. 47, No. 6, June 2009.
  12. Chen, J-P, Johnson, B., Hathaway, M.D., and Webster, R.S., “Flow Characteristics of Tip Injection on Compressor Rotating Spike via Time-Accurate Simulation,” Journal of Propulsion and Power, Vol. 25, No. 3, May-June, 2009, pp. 678-687.
  13. Boelens, O.J., Badcock, K.J., Görtz, S., Morton, S., Fritz, W., Karman, Jr., S.L., Michal, T., and Lamar, J.E., “F-16XL Geometry and Computational Grids Used in Cranked Arrow Wing Aerodynamics Project International,”Journal of Aircraft, Vol. 46, No. 2, March–April 2009, pp. 369-376.
  14. Kapadia, S. and Anderson, W.K., “Sensitivity Analysis for Solid Oxide Fuel cells using a Three-Dimensional Numerical Model,” Journal of Power Sources, Volume 189, Issue 2, April, 2009, Pages 1074-1082
  15. 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.
  16. 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.
  17. Karman, Jr., S.L., and Sahasrabudhe, M., “Unstructured Elliptic Smoothing Revisited,” 47th Aerospace Sciences Meeting and Exhibit, January 5th - January 9th, 2009, Orlando, Florida, AIAA-2009-1362.
  18. Wang, Li and Mavriplis, Dimitri J., “Adjoint-based h-p Adaptive Discontinuous Galerkin Methods for the Compressible Euler Equations,” 47th AIAA Aerospace Science Meeting, January 2009, Orlando, FL, AIAA-2009-0952.

2008 (back to top)

  1. Sivakumar, P., Hyams, D.G., Taylor, L.K., and Briley, W.R., “Primitive-Variable Riemann Fluxes for Solution of the Shallow Water Equations with Embedded Wet/Dry Interfaces,” UTC-CECS-SimCenter-2008-06, November 2008.
  2. 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 Fluid-Structure Interaction,” Proceedings of the 27th ONR Symposium on Naval Hydrodynamics, Seoul, Korea, 5-10 Oct. 2008.
  3. 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, 5-10 Oct. 2008.
  4. Lee, D., Maki, K., Wilson, R., Troesch, A., and Vlahopoulos, N., “Dynamic Response of a Marine Vessel Due to Wave-Induced Slamming,” Int. Sym. On Vibro-Impact Dynamics of Ocean Systems and Related Problems, Troy, Michigan, 2-3 Oct. 2008.
  5. 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.
  6. Briley, W. Roger and McDonald, H., “Reflections on the Evolution of Implicit Navier-Stokes Algorithms,” UTC-CECS-SimCenter-2008-04, September 2008.
  7. Wilson, Robert V., “A Review of Computational Ship Hydrodynamics,” UTC-CECS-SimCenter-2008-03, September 2008.
  8. Anderson, W. Kyle, Karman, Jr., S.L., and Burdyshaw, Chad, “Geometry Parameterization Using Control Grids,” AIAA 2008-Presented at the 12th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, Victoria, BC, September 10-12, 2008.
  9. Lange, K. and Anderson, W.K. “Sensitivity Derivatives for Plasma Discharge Simulations.” AIAA-2008-5930. 12th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, September 2008.
  10. Sahasrabudhe, M., “Unstructured Mesh Generation and Manipulation based on Elliptic smoothing and Optimization,” Ph.D. Dissertation, University of Tennessee at Chattanooga, August 2008.
  11. Kapadia, S., Anderson, W. K., and Elliott, L., “Sensitivity Analysis of Three-Dimensional Solid Oxide Fuel Cell Model,” 6th International ASME Conference on Fuel Cell Science, Engineering, and Technology, Denver, June 16-18, 2008.
  12. Whitfield, D.L, Pankajakshan, R., Sreenivas, K., and, Taylor, L.K. “Numerical Derivatives, Matrix-Vector Product, and Richardson Extrapolation Using Complex Variables,” UTC-CECS-SimCenter-2008-01, March 2008.
  13. Hajjawi, M., Taylor, L., and Nichols, III, D.S., “Assessment and Modification for Reynolds Stress Transport Turbulence Model Flow Prediction,” AIAA-2008-0568, 46th AIAA Aerospace Sciences Meeting and Exhibit, January 2008.
  14. Hajjawi, M., Taylor, L., and Nichols, III, D.S., “Assessment of Filtered Based RANS Turbulence Model for Unsteady Separated Flow Prediction,” AIAA-2008-0670, 46th AIAA Aerospace Sciences Meeting and Exhibit, January 2008.
  15. Karman, Jr., S.L. and Betro, V., “Parallel Hierarchical Unstructured Mesh Generation with General Cutting,” AIAA-2008-0918, Reno, NV, Jan. 2008.

2007 (back to top)

  1. Burdyshaw, C.E. and Anderson, W.K., “Advances in Discrete Sensitivity Methods Applied to Uncertainty Analysis NATO Research and Technology Organisation,” RTO-MP-AVT-147, Conference on Computational Uncertainty in Military Vehicle Design, Papers presented at the RTO Applied Vehicle Technology Panel (AVT) Symposium held in Athens, Greece on 3-6 December 2007.
  2. 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. 1445-1459.
  3. Pankajakshan, Ramesh, Sreenivas, Kidambi, Mitchell, Brent, and Whitfield, David L., “CFD Simulations of Class 8 Trucks,” 2007-01-4293, SAE 2007 Commercial Vehicle Engineering Congress & Exhibition, October 2007.
  4. Pankajakshan, R., Mitchell, B. and Whitfield, D., “Full-Scale 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. 339-348. 2009.
  5. Sreenivas, K., Mitchell, B., Nichols, III, D.S., Hyams, D.G., and Whitfield, D.L., “Computational Simulation of the GCM Tractor-Trailer Configuration,” Aerodynamics of Heavy Vehicles II: Trucks, Buses, and Trains, Lake Tahoe, August 2007.
  6. 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, 5-8 Aug. 2007.
  7. Kapadia, S., Anderson, W.K., Elliott, L, and Burdyshaw, C., “Adjoint method for solid-oxide fuel cell simulations,”Journal of Power Sources, Vol. 166, 2007, pp. 376-385.
  8. Arabshahi, A. and Whitfield, D. L., “Computational of Dynamic Stability and Control Derivatives,” THEC Final Report, January 2005 – July 2007.
  9. Arabshahi, A., Webster, R. S., Briley, W. R., and Whitfield, D. L., “Advancement and Verification of the Navier-Stokes Flow Solver for Rocket Motor Internal Flows,” THEC Final Report, July 2005 – June 2007.
  10. 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 2007-4832.
  11. 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, FuelCell2007-25157.
  12. 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. 419-451.
  13. Carrica, P., Wilson R., and Stern F., “An Unsteady Single-Phase Level Set Method for Viscous Free Surface Flows,” Vol. 53, No. 2, Int. J. of Num. Methods Fluids , Jan. 2007, pp. 229-256.
  14. 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,” AIAA-2007-1449, 45th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, Jan. 8-11, 2007.
  15. Karman, Jr., S.L. and Sahasrabudhe, M., “Unstructured Adapted Elliptic Smoothing,” AIAA-2007-0559, 45th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, Jan. 8-11, 2007.
  16. Karman, Jr., S.L., Mitchell, B., Sawyer, S., and Whitt, J., “Unstructured Grid Solutions of CAWAPI F-16XL by UT SimCenter,” AIAA-2007-0681, 45th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, Jan. 8-11, 2007.
  17. Sreenivas, K., Nichols, III, D.S., Hyams, Mitchell, B., Sawyer, S., and Whitfield, D.L., “Computational Simulation of Heavy Trucks,” AIAA-2007-1087, 45th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, Jan. 8-11, 2007.
  18. 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,” AIAA-2007-1088, 45th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, Jan. 8-11, 2007.
  19. Pankajakshan, R., Mitchell, B.J., and Taylor, L.K., “Simulation of Unsteady Two-Phase Flows using a Parallel Eulerian-Lagrangian Approach,” AIAA-2007-0340, 45th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, Jan. 8-11, 2007.
  20. Nichols, III, D.S., Sreenivas, K., Karman, Jr., S.L., and Mitchell, B., “Turbulence Modeling for Highly Separated Flows,” AIAA-2007-1407, 45th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, Jan. 8-11, 2007.
  21. Karman, Jr., S.L., “Unstructured Viscous Layer Insertion Using Linear-Elastic Smoothing,” AIAA Journal, Volume 45, Number 1, pp. 168-180, January 2007.

2006 (back to top)

  1. Tahara, Y., Wilson, R., Carrica, P., and Stern, F., “RANS Simulation of a Container Ship Using a Single-Phase Level Set Method with Overset Grids and the Prognosis for Extension to Self-Propulsion Simulator,” Vol. 11, No. 4, J. Marine Science and Technology, 2006, pp. 209-228.
  2. Almeida, T.G., Walker, D.T., Leighton, R.I., Alajbegovic, A., Pankajakshan, R., Taylor, L.K., Whitfield, D.L., and Ceccio, S.L., “A Reynolds-Averaged Model for the Prediction of Friction Drag Reduction by Polymer Additives,” 26th Symposium on Naval Hydrodynamics, Rome Italy, September. 17-22, 2006.
  3. Carrica, P.M., Wilson, R.V., Noack, R., Xing, T., Kandasamy, M., Shao, J., Sakamoto, N., and Stern, F., “A Dynamic Overset, Single-Phase Level Set Approach for Viscous Ship Flows and Large Amplitude Motions and Maneuvering,” 26th Symposium on Naval Hydrodynamics, Rome Italy, September. 17-22, 2006.
  4. 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. 17-22, 2006.
  5. Arabshahi, A., Webster, R.S., Briley, W.R., and Whitfield, D. L., “Numerical Analysis of Solid Propellant Rocket Motor Internal Flows,” AIAA-2006-5114, July, 2006.
  6. Sreenivas, K., Taylor, L., and Briley, W.R.,“A Global Preconditioner for Viscous Flow Simulations at All Mach Numbers,” AIAA-2006-3852, June 2006.
  7. 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. 1277-1286, June 2006.
  8. Hyams, D., Sreenivas, K., and Whitfield, D.L., “Parallel FAS Multigrid for Arbitrary Mach Number, High Reynolds Number Unstructured Flow Solvers,” AIAA-2006-2821, June 2006
  9. Nichols, III, D.S., Mitchell, B., Sreenivas, K., Taylor, L., Whitfield, D.L., and Briley, W.R., “Aerosol Propagation in an Urban Environment,” AIAA 2006-3726, June 2006.
  10. Burdyshaw, C.E., “Achieving Automatic Concurrency Between Computational Field Solvers and Adjoint Sensitivity Codes,” Ph.D. Dissertation, University of Tennessee at Chattanooga, May 2006.
  11. 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.501-524, 2006.
  12. Carrica, P., Wilson R., and Stern F., “Unsteady RANS Simulation for Forward Speed Diffraction of a Surface Combatant,” Computers & Fluids, Vol. 35, p.545-570, 2006.
  13. Wilson, R., Carrica, P., and Stern F., “URANS Simulation for a High-Speed Transom Stern Ship with Breaking Waves,” Int. J. of CFD, Vol. 20, No. 2, Feb. 2006, pp.105-125.
  14. 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.
  15. Sahasrabudhe, M., Karman, Jr., S.L., and Anderson, W.K., “Grid Control of Viscous Unstructured Meshes Using Optimization,” AIAA-2006-532, 44th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, Jan. 9-12, 2006.
  16. Ellis, D., Karman, Jr., S.L., and Novobilski, A., Haimes, R., “3D Visualization and Manipulation of Geometry and Surface Meshes,” AIAA-2006-944, 44th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, Jan. 9-12, 2006.
  17. Nichols, III, D.S., Hyams, D., Sreenivas, K., Mitchell, B., Taylor, L., and Whitfield, D., “An Unstructured Incompressible Multi-Phase Solution Algorithm,” AIAA-2006-1290, 44th AIAA Aerospace Sciences Meeting and Exhibit, January 2006.
  18. Sreenivas, K., Pankajakshan, R., Nichols, III, D.S., Mitchell, B., Taylor, L., and Whitfield, D.L., “Aerodynamic Simulation of Heavy Trucks with Rotating Wheels,” AIAA-2006-1394, 44th AIAA Aerospace Sciences Meeting and Exhibit, January 2006.
  19. 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,” AIAA-2006-0418, January 2006.

2005 (back to top)

  1. 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. 336-346, 2005.
  2. 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.
  3. 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 27-30, 2005, Saint-Petersburg, Russia.
  4. Wilson, R. and Stern, F., “URANS Simulations For A High-Speed Transom Stern Ship With Breaking Waves,”Proceedings of FAST 2005, 8th Int. Conf. on Fast Sea Transportation, June 27-30, 2005, Saint-Petersburg, Russia.
  5. 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. 80-97.
  6. 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 Self-Propulsion Simulator,” Proceedings of the CFD Workshop Tokyo 2005, Tokyo, Japan, 9-11, March 2005.
  7.  Miller, R. Wilson, R., Carrica, P., and Gorski, J., “RANS Simulation of a Naval Surface Combatant Using a Single-Phase Level Set Method with Overset Grids,” Proceedings of the CFD Workshop Tokyo 2005, Tokyo, Japan, 9-11, March 2005.
  8. 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.
  9. 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.
  10. Kandasamy, M., Xing, T., Wilson, R., and Stern, F., “Vortical and Turbulent Structures and Instabilities in Unsteady Free-Surface Wave Induced Separation,” Proceedings of 5th Osaka Colloquium, March 14-15, 2005, Osaka Japan.
  11. Taylor, L.K., Pankajakshan, R., Briley, W.R., and Whitfield, D. L., “Scalable Parallel Implicit Algorithm for Advanced Turbulence Closures,” AIAA Paper No. 2005-0876, 43rd Aerospace Sciences Meeting and Exhibit, Reno, NV, January 2005.
  12. 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. 2005-0325, 43rd Aerospace Sciences Meeting and Exhibit, Reno, NV, January 2005.
  13. Burdyshaw, C.E. and Anderson, W.K., “A General and Extensible Unstructured Mesh Adjoint Method,” AIAA Paper No. 2005-0335, 43rd Aerospace Sciences Meeting and Exhibit, Reno, NV, January 2005.

2004 (back to top)

  1. Arabshahi, A. and Janus, J.M., “A Multiblock Compressible Navier-Stokes Flow Solver Applied to Complex Launch Vehicles,” AIAA Journal of Spacecraft and Rockets, Vol. 41, No. 3, pp. 469-472, May-June 2004.
  2. Karman, Jr., S.L., “Hierarchical Unstructured Mesh Generation,” AIAA Paper No. 2004-0613, 42nd Aerospace Sciences Meeting and Exhibit, Reno, NV, January 2004.
  3. 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.
  4. Wilson, R., Shao, J., and Stern, F., “Discussion: “Criticisms of the “Correction Factor” Verification Method” (Roache, P., 2003, ASME J. Fluids Eng., 125, pp. 732-733),” ASME J. Fluids Eng, Vol. 126, No. 4, 2004.
  5. Wilson, R., Carrica, P., Hyman, M., and Stern, F., “A Steady and Unsteady Level-Set Method for Large Amplitude Ship Motions and Maneuvering,” Proceedings 25th ONR Symposium on Naval Hydrodynamics, St. Johns, Canada, August 2004.
  6. 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), Kirkenes-Bergen, Norway, 19-24 April 2004.
  7. Xing, T., Kandasamy, M., Wilson, R. and Stern, F., “DES and RANS of Unsteady Free-surface Flows,” 42nd AIAA Aerospace Sciences Meeting, Reno, Nevada, 5-8 Jan 2004, Division for Fluid Dynamics.

2003 (back to top)

  1. 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.
  2. Briley, W.R., Taylor, L.K., and Whitfield, D.L., “High-Resolution Viscous Flow Simulations at Arbitrary Mach Number,” Journal of Computational Physics, 184(1):79-105, 2003.
  3. 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. 605-621.
  4. Sreenivas, K., Cash, A.N., Hyams, D.G., and Taylor, L.K., “Computational Study of Propulsor-Hull Interactions,” AIAA Paper No. 2003-1262, 41st Aerospace Sciences Meeting and Exhibit, Reno, NV, January 2003.
  5. Blades, E., Sreenivas, K., and Hyams, D.G., “Arbitrary Overlapping Interfaces for Unsteady Unstructured Parallel Flow Simulations,” AIAA Paper No. 2003-0276, 41st Aerospace Sciences Meeting and Exhibit, Reno, NV, January 2003.
  6. Pankajakshan, R., Taylor, L.K., Briley, W. R., and Whitfield, D.L., “Arbitrary Mach Number Flow Simulations,” AIAA Paper No. 2003-1236, 41st Aerospace Sciences Meeting and Exhibit, Reno, NV, January 2003.
  7. Hindi, M.M., White, C.A., and Kozub, R.L., “Double K-shell ionization probability in Mn54,” Physical Review C 68, 014306 (2003), July 25, 2003.
  8. 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.
  9. 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.
  10. Stern, F., Wilson, R., and Shao, J., “Statistical Approach to CFD Code Certification,” AIAA 2003-6345, Applied Aerodynamics Special Session on CFD Uncertainty, 41st Aerospace Sciences Meeting, Reno, Nevada, 6-9 January 2003.

2002 (back to top)

  1. Lucien, V., Alpuche-Aviles, M. A., Graves-Brook, 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 22-27, 2002.
  2. Nichols, III, D.S., “Development of a Free Surface Method Utilizing an Incompressible Multi-Phase Algorithm to Study the Flow About Surface Ships and Underwater Vehicles,” PhD Dissertation, Mississippi State University, August 2002.
  3. Arabshahi, A. and Gibeling, H. J., “Computational Hydrodynamics for an Autonomous Underwater Vehicle with Moving Control Surfaces,” FEDSM2002-31428, ASME 2002 Fluids Engineering Division Summer Meeting, Montreal, Canada, July 2002.
  4. 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.
  5. 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.
  6. Burg, C. O. E., Sreenivas, K., Hyams, D. G., and Mitchell, B., “Unstructured Nonlinear Free Surface Flow Solutions: Validation and Verification,” AIAA Paper No. 2002-2977, 32nd AIAA Fluid Dynamics Conference and Exhibit, St. Louis, MO, June 2002.
  7. 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. 2002-3306, 32nd AIAA Fluid Dynamics Conference and Exhibit, St. Louis, MO, June 2002.
  8. Blades, E.L., Marcum, D., and Mitchell, B., “Simulation of Spinning Missile Flow Fields Using U2NCLE,” AIAA Paper No. 2002-2797, 32nd AIAA Fluid Dynamics Conference and Exhibit, St. Louis, MO, June 2002.
  9. Eglin, J.L., Dequeant, M.Q., Graves-Brook, M.K., and Smith, L.T., “Hydrolysis of Cyanophenols at Bimetallic Re2(III,III) Core,” Abstracts of Papers, 223rd ACS National Meeting, April 7-11, 2002.
  10. Blades, E.L., Marcum, D.L., and Mitchell, B., “Euler and Navier-Stokes Simulation of the Aerodynamics of a Spinning Missile with Dithering Control Surfaces.” MSSU-COE-ERC-02-02, Mississippi State University, Feb. 2002.
  11. 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. 181-195, 2002.
  12. Briley, W.R, Keynote Address: Computational Fluid Dynamics and Computational Engineering Education. Forum on Advances in Fluids Engineering Education, FEDSM2002-31378, ASME Joint U.S.-European Fluids Engineering Division Summer Meeting, Montreal, Canada, July 2002.
  13. Pankajakshan, R., Remotigue, M.G., Taylor, L.K., Jiang, M., Briley, W.R., and Whitfield, D.L., “Validation of Control-Surface Induced Submarine Maneuvering Simulations Using UNCLE,” 24th Symposium on Naval Hydrodynamics, Fukuoka, Japan, July 8-13, 2002.
  14. Chen, J.-P., and Briley, W.R, “Development of a Parallel Turbomachinery Flow Solver,” MSSU-COE-ERC-02-109 (NASA Grant NAG3-2176), June 2002.
  15. 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, “Physics-Based Maneuvering Simulations for Tiltrotor Aircraft,” MSU Report No. MSSU-COE-ERC-02-06 (NASA-ARC Grant NAG2-1232), April 2002.
  16. 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. MSSU-COE-ERC-02-09 (ONR Grant N00014-99-1-0751), May 2002.
  17. Burg, C.O.E., Sreenivas, K., and Hyams, D.G., “Unstructured Nonlinear Free Surface Simulations for the Fully-Appended DTMB Model 5415 Series Hull Including Rotating Propulsors,” 24th Symposium on Naval Hydrodynamics, Fukaoka, Japan, July 2002.
  18. 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 8-13, 2002.
  19. 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.
  20. 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 time-dependent Schrodinger equation,” Journal of Molecular Structure (Theochem), Vol. 592, pp. 69-77, 2002.
  21. 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. 1155-1163.
  22. Rumsey, C.L., Gatski, T.B., Anderson, W.K., and Nielsen, E.J., “Isolating Curvature Effects in Computing Wall-Bounded Turbulent Rows,” Intl. J. Heat and Fluid Flow, Vol. 22, 2002, pp. 573-582.
  23. Stern F., and Wilson, R., “Author’s Closure,” ASME J. Fluids Eng., Vol. 124(3), 2002, pp.810-811.
  24. 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 8-13, 2002.
  25. 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 2002-0904, Jan. 2002.

2001 (back to top)

  1. Grayson, B. A., Wolan, J. T., Graves-Brook, M. K., Bledsoe, M., Kirchner, K., Saddow, S. E., "Comparison of 3C-SiC films grown by CVD on Si(111) and Si(211) substrates," Materials Research Symposium Proceedings (2001), 604(Silicon Carbide: Materials, Processing and Devices).
  2. Nelson, A. E., Graves-Brook, M. K., Schulz, K. H., "Analysis of Cerium-Zirconium Mixed Metal Oxides by X-Ray Phtoelectron Spectroscopy," Surface Science Spectra (2001), 8(2), 126-161.
  3. 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.
  4. Briley, W. R. and H. McDonald: An Overview and Generalization of Implicit Navier-Stokes Algorithms and Approximate Factorization. Journal of Computers and Fluids, Vol. 30, pp. 807-828, 2001.
  5. Marcum, D., Mitchell, B., Sreenivas, K., and Hyams, D., "Unstructured Grid Generation for Large-Scale CFD Applications," ECCOMAS Computational Fluid Dynamics Conference 2001, University of Wales, Swansea, Wales, UK, September 2001 (Invited).
  6. 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.
  7. Stern F., Wilson R., Coleman H., and Paterson E., “Comprehensive Approach to Verification and Validation of CFD Simulations-Part 1: Methodology and Procedures,” ASME J. Fluids Eng., Vol. 123, Dec. 2001, pp. 793-802.
  8. Wilson R., Stern F., Coleman H., and Paterson E., “Comprehensive Approach to Verification and Validation of CFD Simulations-Part2: Application for RANS Simulation of A Cargo/Container Ship,” ASME J. Fluids Eng., Vol. 123, Dec. 2001, pp. 803-810. Sivakumar, P., "Numerical Investigation of a Single Elliptic Impinging Jet", M.S. Thesis, Louisiana Tech University, November 2001.
  9. Donatello, D., Sreenivas, K., and Taylor, L.K., “Computations of Unsteady Forces and Moments for SUBOFF Undergoing Prescribed Maneuvers Using U2NCLE,” MSSU-COE-ERC-01-12, Mississippi State University. October 2001.
  10. Lorenzo, L., Sreenivas, K., Mitchell, B., and Taylor, L.K., “Computation of Forces and Moments for the Airship AKRON and SUBOFF Using U2NCLE,” MSSU-COE-ERC-01-11, Mississippi State University, October 2001.
  11. Hyams, D.G., Sreenivas, K., Taylor, L.K., and Whitfield, D.L., “Incompressible Unstructured RANS Simulations for a Low Speed Centrifugal Compressor using U2NCLE,” MSSU-COE-ERC-01-10, Mississippi State University, October 2001.
  12. Newman, J.C., and Whitfield, D.L., "Sensitivity Derivative Analysis for Use in Computational Design," MSU Report MSSU-COE-ERC-01-06, Sept. 2001.
  13. 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. 263-271, 2001.
  14. Burdyshaw, Chad, "Quasi 3D Multi-Stage Turbomachinery Pre-Optimizer," M.S. Thesis, Mississippi State University, August 2001.
  15. Graves-Brook, Melissa, K., "Reactivity Studies of Dirhenium Octachloride (IV,IV) with Nitriles," M.S. Thesis, Department of Chemistry, Mississippi State University, August 2001.
  16. Marcum, D., Mitchell, B., Sreenivas, K., and Hyams, D., "Unstructured Grid Generation for Large-Scale CFD Applications," 1st MIT Conference on Computational Fluid and Solid Mechanics, Massachusetts Institute of Technology, Cambridge, MA, June 2001 (Invited)
  17. Chen, J. P., and Briley, W. R., "A Parallel Flow Solver for Unsteady Multiple Blade Row Turbomachinery Simulations". ASME Paper 2001-GT-0348, presented at ASME TURBO EXPO 2001, New Orleans, LA, June 2001.
  18. Webster, R.S., "A Numerical Study of the Conjugate Conduction-Convection Heat Transfer Problem", Ph.D. Dissertation, Mississippi State University, May 2001.
  19. 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.
  20. Wilson R., Demuren A., and Carpenter M., “Higher-Order Compact Schemes for Numerical Simulation of Incompressible Flows, Part II: Applications”, Numerical Heat Transfer, Part B, 39(3), March 2001, pp. 231-255.
  21. Demuren A., Wilson R., and Carpenter M., “Higher-Order Compact Schemes for Numerical Simulation of Incompressible Flows, Part I: Theoretical Development”, Numerical Heat Transfer, Part B, 39(3), March 2001, pp. 207-230.
  22. Briley, W. R., Taylor, L. K., and Whitfield, D. L., "High-Resolution Viscous Flow Simulations at Arbitrary Mach Number," Submitted to Journal of Computational Physics (also MSU Report No. MSSU-COE-ERC-01-04, March 2001).
  23. Briley, W., Taylor, L., and Whitfield, D., "Scalable Flow Simulations with Rotating Components," Navigator, Naval Oceanographic Office: Major Shared Resource Center, Spring 2001, pp. 4-7.
  24. 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 2001-0682, 39th Aerospace Sciences Meeting Conference and Exhibit, Reno, NV, January 2001.
  25. 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 2001-1093, 39th Aerospace Sciences Meeting Conference and Exhibit, Reno, NV, January 2001.
  26. Nielsen, E. J., and Anderson, W. K., "Recent Improvements in Aerodynamic Design Optimization on Unstructured Meshes," AIAA 01-0596, Jan., 2001.
  27. Anderson, W. K., Newman, J. C., Whitfield, D. L., and Nielsen, E. J., "Sensitivity Analysis for Navier-Stokes Equations on Unstructured Meshes using Complex Variables," AIAA Journal, Vol. 398, No. 1, pp.56-63, January 2001.

2000 (back to top)

  1. 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.
  2. Chen, J., and Whitfield, D., "Computation of Rotor-Stator Interaction Using the Navier-Stokes Equations (NASA Grant NAG3-1712, Final Report)," MSSU-COE-ERC-00-12, October 2000.
  3. 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.
  4. 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 17-22, 2000.
  5. 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 17-22, 2000.
  6. 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. 14-16, 2000.
  7. 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.
  8. 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.
  9. Sheng, C., Hyams, D., Sreenivas, K., Gaither, A., Marcum, D., and Whitfield, D., "Three-Dimensional Incompressible Navier-Stokes Flow Computations About Complete Configurations Using a Multiblock Unstructured Grid Approach," MSSU-COE-ERC-00-07, July, 2000.
  10. Hyams, D.G , "An Investigation of Parallel Implicit Solution Algorithms for Incompressible Flows On Unstructured Topologies," Ph.D. Dissertation, Mississippi State University, May 2000.
  11. 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. 2000-0271, Reno, NV, January 2000.
  12. 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.
  13. Pankajakshan, R., Taylor, L.K., Jiang, M., Remotigue, M.G., Briley, W.R., and Whitfield, D.L., "Parallel Simulations for Control-Surface Induced Submarine Maneuvers," Proc., 38th Aerospace Sciences Meeting & Exhibit, AIAA Paper No. 2000-0962, Reno, NV, January 2000.
  14. Arabshahi, A., Gibeling H. J., “Numerical Simulation of Viscous Flows about Underwater Vehicles,” OCEANS 2000 MTS/IEEE Conference & Exhibition, Providence, RI, September 2000.
  15. 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.
  16. Karman, Jr., S.L., Domel, N.D., “SPLITFLOW: Progress in 3 D CFD with Cartesian Omni-Tree Grids for Complex Geometries”, AIAA 2000-1006, 2000.
  17. Alexandrov, N. M., Nielsen, E. J., Lewis, R. M., and Anderson, W K., "Model Management with Variable-Fidelity Physics Applied to Multi-element Airfoil Optimization," AIAA 00-4886, Sept., 2000.
  18. 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)

  1. 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 19-22, 1999.
  2. 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. 99-3101, June 1999.
  3. Anderson, W.K., Whitfield, D.L., Newman III, J.C., Nielsen, E.J., "Sensitivity Analysis for the Navier-Stokes Equations on Unstructured Meshes Using Complex Variables," Proc., 14th AIAA Computational Fluid Dynamics Conference, AIAA Paper No. 99-3294, June 1999.
  4. Janus, J. M., Horstman, H. S., and Whitfield, D.L., "Unsteady Flowfield Simulation of Ducted Prop-Fan Configurations," Journal of Propulsion and Power, Vol. 15, No. 1, January-February 1999, pp. 64-72.
  5. Arabshahi, A. and Janus, J. Mark, "A Multiblock Compressible Navier-Stokes Flow Solver Applied to Complex Launch Vehicles," AIAA-99-3378, June 28 - July 1, 1999.
  6. Sheng, C., Hyams, D., Sreenivas, K., Gaither, J.A., Marcum, D. L., Whitfield, D.L. and Anderson, W.K., "Three-Dimensional Incompressible Navier-Stokes Flow Computations About Complete Configurations Using a Multi-Block Unstructured Grid Approach," AIAA-99-0778, 37th AIAA Aerospace Sciences Meeting, Reno, NV, January 1999.
  7. Arabshahi, A., Janus, J. M., “ A Multiblock Compressible Navier-Stokes Flow Solver Applied to Complex Launch Vehicles,” AIAA-99-3378, the 14th Computational Fluid Dynamics Conference, Norfolk, VA, June 1999.
  8. Arabshahi, A., Gibeling H. J., “Computational Hydrodynamics for Autonomous Underwater Vehicles,” the 4th Mississippi State Conference on Differential Equations & Computational Simulations, May 1999.
  9. 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 Navier-Stokes Equations," AIAA 99-0785, January, 1999.
  10. Anderson, W. K., and Bonhaus, D. L., "Airfoil Design on Unstructured Grids for Turbulent Rows," AIAA Journal, Vol. 37, No. 2, Feb. 1999, pp. 185-191.
  11. 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. 169-176.
  12. 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.
  13. Nielsen, E. J., Anderson, W K., "Aerodynamic Design Optimization on Unstructured Meshes Using the Navier-Stokes Equations," AIAA Journal, Vol. 37, No. 11, Nov. 1999, pp. 1411-1419.
  14. 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. 957-964.
  15. Anderson, W Kyle, and Venkatakrishnan, V, "Aerodynamic Design Optimization on Unstructured Grids with a Continuous Adjoint Formulation," Computers and Fluids, Vol. 28, No. 4-5, 1999, pp.443-480.
  16. 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.
  17. Demuren A., Wilson R., “Streamwise Vorticity Generation in Laminar and Turbulent Jets”, Proceedings of the 3rd ASME/JSME Joint Fluids Engineering Conference, FEDSM99-6807, San Francisco, July 18-23, 1999.
  18. 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, FEDSM99-6913, San Francisco, July 18-23, 1999.
  19. Eglin J. L., Graves-Brook, M. K., "Reactivity of the Re2(III,III) core with substituted nitriles," Abstracts of Papers, 218th ACS National Meeting, August 22-26 (1999).

1998 (back to top)

  1. 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.
  2. 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 9-14, 1998.
  3. Beggs, J. H., and W. R. Briley, "An Implicit Characteristic Based Method for Computational Electromagnetics," Report MSSU-COE-ERC-98-11, August, 1998. Submitted to J. Applied Computational Electromagnetics Society.
  4. Newman, J.C., Anderson, W.K., and Whitfield, D.L., "Multidisciplinary Sensitivity Derivatives Using Complex Variables," MSSU-COE-ERC-98-08, July 1998.
  5. Whitfield, D.L., and Taylor, L.K., "Variants of a Two-Level Method for the Approximate Numerical Solution of Field Simulation Equations," MSSU-EIRS-ERC-98-09, July 1998.
  6. Sreenivas, K. and Whitfield, D.L., "Time-and Frequency-domain Numerical Simulation of Linearized Euler Equations," AIAA Journal, Vol. 36, No. 6, June 1998, pp. 968-975.
  7. 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., "Large-Scale Simulations for Maneuvering Submarines and Propulsors," AIAA Paper No. 98-2930, 29th AIAA Plasmadynamics and Lasers Conference, Albuquerque, NM, June 15-18, 1998.
  8. 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 Navier-Stokes Equations," Presented in the Third Osaka Colloquium on Advanced CFD Applications to Ship Flow and Hull Form Design, Osaka, Japan, May 25-27, 1998.
  9. Busby, J.A., Taylor, L. K., Jiang, M.Y., and Whitfield, D.L., "Unsteady 3-D Incompressible Flow Interaction in Multiple Blade-Row Turbomachinery," AIAA Paper No. 98-0423, AIAA 36th Aerospace Sciences Meeting and Exhibit, Reno, NV, January 12-15, 1998.
  10. Beddhu, M., Jiang, M-Y., 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. 67-84, 1998.
  11. Arabshahi, A., et. al., “A Perspective on Naval Hydrodynamic Flow Simulations,” The 22nd Naval Hydrodynamics Program, August 1998.
  12. 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 Navier-Stokes Equations.” Submitted for publication in Journal of Computational Physics, April 1998.
  13. Webster, R. S., ‘‘Numerical Study of Base Flow Induced by Exhaust Plume Impingement’’, AIAA-98-3621, July, 1998.
  14. 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.
  15. Wilson R., Demuren A., “Numerical Simulation of Turbulent Jets with Rectangular Cross-Section”, Journal of Fluids Engineering, 120, June 1998, pp. 285-290.
  16. 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 9-14, 1998.
  17. Wilson R. and Demuren A., “On the Origin of Streamwise Vorticity in Complex Turbulent Jets”, Proceedings of the ASME Fluids Engineering Division Summer Meeting, FEDSM98-5004, Washington D.C., June 21-25, 1998.
  18. 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.
  19. Eglin, J. L., Graves-Brook, 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 29-April 2 (1998).

1997 (back to top)

  1. Pankajakshan, R., "Parallel Solution of Unsteady Incompressible Viscous Flows using Multiblock Structured Grids," Ph.D. Dissertation, Mississippi State University, Dec. 1997.
  2. 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.
  3. Sheng, C., Whitfield, D.L. and Anderson, W.K., "A Multiblock Approach for Calculating Incompressible Fluid Flows on Unstructured Grids," AIAA Paper No. 97-1866, 13th AIAA Computational Fluid Dynamics Conference, Snowmass, CO, June 1997.
  4. 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 Navier-Stokes Equations," Presented at the ONR Ship Hydrodynamics Workshop, David Taylor Model Basin, Carderock, MD, June 2-3, 1997.
  5. Davoudzadeh, F., Taylor, L. K., Zierke, W. C., Dryer, J. J., McDonald, H. and Whitfield, D. L., "Coupled Navier-Stokes and Equations of Motion Simulation of Submarine Maneuvers, Including Crashback," FEDSM97-3129, 1997 ASME Fluids Engineering Division Summer Meeting, Vancouver, British Columbia, Canada, June 22-26, 1997.
  6. Dryer, J. J., Taylor, L. K., Zierke, W. C. and Davoudzadeh, F., "A First-Principle Approach to the Numerical Prediction of the Maneuvering Characteristics of Submerged Bodies," FEDSM97-3130, 1997 ASME Fluids Engineering Division Summer Meeting, Vancouver, British Columbia, Canada, June 22-26, 1997.
  7. Beddhu, M., Jiang, M-Y., 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," MSSU-EIRS-ERC-97-5, March 1997.
  8. 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. 161-168, 1997.
  9. Chen, J. P., Ghosh, A. R., Sreenivas, D., and Whitfield, D. L., "Comparison of Computations Using Navier-Stokes Equations in Rotating and Fixed Coordinates for Flow Through Turbomachinery," AIAA Paper No. 97-0878, AIAA 35th Aerospace Sciences Meeting and Exhibit, Reno, NV, January 6-10, 1997.
  10. 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. 97-0624, AIAA 35th Aerospace Sciences Meeting and Exhibit, Reno, NV, January 6-10, 1997.
  11. Sheng, C., Chen, J.P., Taylor, L. K., Jiang, M.Y., and Whitfield, D.L., "Unsteady Multigrid Method for Simulating 3-D Incompressible Navier-Stokes Flows on Dynamic Relative Motion Grids," AIAA Paper No. 97-0446, AIAA 35th Aerospace Sciences Meeting and Exhibit, Reno, NV, January 6-10, 1997.
  12. 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 Physics-Based Means of Computing the Flow Around a Maneuvering Underwater Vehicle," Technical Report No. TR 97-002, Applied Research Laboratory, Penn State University, January 1997.
  13. 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. 2-3, pp. 205-215, 1997.
  14. Reed, C.L., Karman, Jr., S.L., “Implementation of Low Speed Preconditioning in the Splitflow Code”, AIAA 97-1867, 1997.
  15. Wilson R. and Demuren A., “Large-Eddy Simulation of Complex Turbulent Jets”, Proceedings of ASME Fluids Engineering Division Summer Meeting, FEDSM97-5214, Vancouver BC, Canada, June 1997.

1996 (back to top)

  1. Beddhu, M., Taylor, L. K., and Whitfield, D. L., "Strong Conservative Form of the Incompressible Navier-Stokes Equations in Rotating Frame with a Solution Procedure," Journal of Computational Physics, Vol. 128, No. 2, October 1996, pp. 427-437.
  2. Whitfield, D. L., "Numerical Solution of the Shallow Water Equations," MSSU-EIRS-ERC-96-4, July 1996.
  3. McDonald, H. and Whitfield, D. L., "Self-Propelled Maneuvering Underwater Vehicles," Twenty-First Symposium on Naval Hydrodynamics, Trondheim, Norway, June 24-28, 1996.
  4. Pankajakshan, R. and W. R. Briley, "Parallel Solution of Viscous Incompressible Flow on Multi-Block 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. 601-608, 1996.
  5. Briley, R., Neerarambam, S.S., and Whitfield, D.L., "Implicit Lower-Upper/Approximate- Factorization Algorithms for Incompressible Flows," Journal of Computational Physics, Vol. 123, March 1996, pp. 32-42.
  6. Sheng, C., Taylor, L.K., Chen, J.P, Jiang, M.Y., and Whitfield, D.L., "Multigrid Computations of 3-D Incompressible Internal and External Viscous Rotating Flows," MSSU-EIRS-ERC-96-1, February 1996.
  7. Finley, D.B., Karman Jr., S.L., "Prediction of Compressibility Effects Using Unstructured Euler Analysis on Vortex Dominated Flow Fields," AIAA 96-2499, 1996.
  8. Wilson R., Demuren A., “Numerical Simulations of Two-Dimensional, Spatially Developing Mixing Layers”,Numerical Heat Transfer, Part A, 29, 1996, pp. 485-509.
  9. Wilson R. and Demuren A., “Numerical Simulation of Turbulent Jets with Rectangular Cross-Section”, Proceedings of the ASME Fluids Engineering Division Summer Meeting, FED-Vol. 238(3), San Diego, California, July 1996, pp. 121-128.

1995 (back to top)

  1. Sheng, C., Taylor, L. K., and Whitfield, D. L., "Multigrid Algorithm for Three-Dimensional Incompressible High-Reynolds Number Turbulent Flows," AIAA Journal, Vol. 33, No. 11, November 1995, pp. 2073-2079.
  2. 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.
  3. 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 3-4, September 1995, ISSN: 1061 8562 IJCCFEC, pp. 307-321.
  4. Sheng, C., Taylor, L. K., and Whitfield, D. L., "A Multigrid Algorithm for Unsteady Incompressible Euler and Navier-Stokes Flow Computations," Sixth International Symposium on Computational Fluid Dynamics, Lake Tahoe, Nevada, September 4-8, 1995.
  5. Briley, W. R., Neerarambam, S. S., and Whitfield, D. L., "Implicit Lower-Upper/Approximate- Factorization Algorithms for Viscous Incompressible Flows," AIAA Paper No. 95-1742 - CP, 12th Computational Fluid Dynamics Conference, San Diego, CA, June 19-22, 1995.
  6. Vanden, K. J. and Whitfield, D. L., "Direct and Iterative Algorithms for the Three-Dimensional Euler Equations,"AIAA Journal, Vol. 33, No. 5, May 1995, pp. 851-858.
  7. Beddhu, M., Jiang, M-Y., 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.
  8. Webster, R. S., Chen, J. P., and Whitfield, D. L., "Numerical Simulation of a Helicopter Rotor in Hover and Forward Flight," AIAA Paper No. 95-0193, AIAA 33rd Aerospace Sciences Meeting and Exhibit, Reno, NV, January 9-12, 1995
  9. Taylor, L. K., Arabshahi, A., and Whitfield, D. L., "Unsteady Three-Dimensional Incompressible Navier-Stokes Computations for a 6:1 Prolate Spheroid Undergoing Time-Dependent Maneuvers," AIAA Paper No. 95-0313,AIAA 33rd Aerospace Sciences Meeting and Exhibit, Reno, NV, January 9-12, 1995.
  10. Arabshahi, A., Taylor, L. K., and Whitfield, D. L., "UNCLE: Toward a Comprehensive Time-Accurate Incompressible Navier-Stokes Flow Solver," AIAA Paper No. 95-0050, AIAA 33rd Aerospace Sciences Meeting and Exhibit, Reno, NV, January 9-12, 1995.
  11. Sheng, C., Taylor, L. K., and Whitfield, D. L., "Multiblock Multigrid Solution of Three-Dimensional Incompressible Turbulent Flow About Appended Submarine Configurations," AIAA Paper No. 95-0203, AIAA 33rd Aerospace Sciences Meeting and Exhibit, Reno, NV, January 9-12, 1995.
  12. Whitfield, D. L., "Perspective on Applied CFD," AIAA Paper No. 95-0349, AIAA 33rd Aerospace Sciences Meeting and Exhibit, Reno, NV, January 9-12, 1995.
  13. 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. 189-198, 1995.
  14. Daiber, M.P., Bomba, Joseph, and Swafford, T.W., “Analysis Method for the Design of Compensated Pitot-static Probes for Use on General Aviation Aircraft,” SAE Technical Paper 951431, 1995 SAE Aerospace Atlantic Conference, May 23-25, 1995, Dayton, Ohio.
  15. Swafford, T.W., Bomba, Joseph, and Daiber, M.P., “Computational Analysis of Compensated Pitot-static Probes Using the Euler Equations,” AIAA-95-1839-CP, AIAA Applied Aerodynamics Conference, San Diego, California, June 1995.
  16. Karman, Jr., S.L., “SPLITFLOW: A 3D Unstructured Cartesian/Prismatic Grid CFD Code for Complex Geometries,” AIAA 95-0434, 1995.
  17. Welterlen, T.J., Karman, Jr., S.L., “Rapid Assessment of F-16 Store Trajectories Using Unstructured CFD,” AIAA 95-0354, 1995.
  18. 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.
  19. 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. 95-2229, June, 1995 (coauthor)

1994 (back to top)

  1. Arabshahi, A., and Pankajakshan, R., “Propulsion/Airframe Interference for Ducted Propfan Engines with Ground Effect,” NASA-CR-197110, November 1994.
  2. 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. 33-48, 1994.
  3. Beddhu, M, Jiang, M-Y., Taylor, L. K., and Whitfield, D. L., "Toward Computation of Ocean Flows Using Navier-Stokes Equations," Supercomputing '94 Proceedings, IEEE Computer Society Press, 1994, pp. 144-153.
  4. Whitfield, D. L., Taylor, L. K., Beddhu, M., and Arabshahi, A., "Discretized Newton-Relaxation Solution of the Three-dimensional Unsteady Incompressible Navier-Stokes Equations," Frontiers of Computational Fluid Dynamics, Chapter 28, pp. 575-594, D.A. Caughey and M. M. Hafez editors, Wiley Publishing, 1994.
  5. Sheng. C., Taylor, L., and Whitfield, D. L., "An Efficient Multigrid Acceleration for Solving the 3-D Incompressible Navier-Stokes Equations in Generalized Curvilinear Coordinates," AIAA-94-2335, 25th AIAA Fluid Dynamics Conference, Colorado Springs, CO, June 1994.
  6. 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.
  7. Hyams, D. G., and Fadel, G. M., "Comparison of Various Move Limit Strategies in Structural Optimization," AIAA Paper 94-1359, 35th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, Hilton Head, SC, April 18-20, 1994.
  8. Whitfield, D. L. and Taylor, L. K., "Numerical Solution of the Two-Dimensional Time-Dependent Incompressible Euler Equations," MSSU-EIRS-ERC-93-14, April 1994.
  9. Swafford, T.W., Loe, D.H., Huff, D.L., Huddleston, D.H., and Reddy, T.S.R., “The Evolution of NPHASE: Euler/Navier-Stokes Computations of Unsteady Two Dimensional Cascade Flow Fields,” AIAA-94-1834-CP, June 1994.
  10. 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. 94-2235, July, 1994 (coauthor)
  11. Demuren A., Wilson R., “Estimating Uncertainty in Computations of Two-Dimensional Separated Flows”, Journal of Fluids Engineering, 216, June 1994, pp. 216-220.

1993 (back to top)

  1. 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. 111-126.
  2. Taylor, L. K., Busby, J. A., Jiang, M. Y., Arabshahi, A., Sreenivas, K., and Whitfield, D. L., "Time Accurate Incompressible Navier-Stokes Simulation of the Flapping Foil Experiment," Proceedings of the Sixth International Conference on Numerical Ship Hydrodynamics, Iowa City, Iowa, August 2-5, 1993, pp. 721-738.
  3. 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. 93-2934, AIAA 24th Fluids Dynamics Conference, Orlando, FL, July 6-9, 1993.
  4. Vanden, K. J. and Whitfield, D.L., "Direct and Iterative Algorithms for the Three-Dimensional Euler Equations," AIAA Paper No. 93-3378, 11th AIAA Computational Fluid Dynamics Conference, Orlando, FL, July 6-9, 1993.
  5. Pankajakshan, R., Arabshahi, A., and Whitfield, D.L., "Turbofan Flowfield Simulation Using Euler Equations with Body Forces," AIAA Paper No. 93-1978, AIAA/SAE/ASME/ASEE 29th Joint Propulsion Conference and Exhibit, Monterey, CA, June 28-30, 1993.
  6. 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.
  7. Cox, C. F., Cinnella, P., and Arabshahi, A., “Multi-Block Calculation for Flows in Local Chemical Equilibrium,” AIAA-93-2999, 24th AIAA Fluid Dynamics Conference, Orlando, FL, July 1993.
  8. 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.
  9. Soni, B. K., Huddleston, D. H., Arabshahi, A., and Vu, B., “A Study of CFD Algorithms Applied to Complete Aircraft Configurations,” AIAA-93-0784, AIAA 31st Aerospace Sciences Meeting, Reno, NV, January 1993.
  10. Swafford, T.W., “Computation of Unsteady Supersonic Quasi-One-Dimensional Viscous-Inviscid Interacting Flow Fields,” AIAA Journal, Vol. 31, No. 2, pp. 404-408, February 1993.
  11. Melnik, R. E., "Applications of a new Wall-Slip Boundary Condition to the computation of Turbulent Flows," presented at the AIAA 24th Fluid Dynamics Conference, Orlando, Fl, AIAA paper No. 93-3108, July, 1993, (coauthor)
  12. Wilson R. and Demuren A., “Estimating Uncertainty in Computations of Two-Dimensional Separated Flows”, Proceedings of the Quantification of Uncertainty in Computational Fluid Dynamics, FED-Vol 158, Washington D.C., June 1993, pp. 9-18.
  13. 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. 679-689.

1992 (back to top)

  1. 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, MSSU-EIRS-ERC-93-1, Mississippi State University, Mississippi State, MS, October 1992.
  2. Janus, J.M., Arabshahi, A., and Whitfield, D.L., "Numerical Solution and Algorithm Analysis for the Unsteady Navier-Stokes Equations on Dynamic Multiblock Grids, Volume I," WL-TR-92-7044, Eglin Air Force Base, FL, October 1992.
  3. Janus, J.M., Cox, C.F., Arabshahi, A., Cinnella, P. C., and Whitfield, D.L., "Numerical Solution and Algorithm Analysis for the Unsteady Navier-Stokes Equations on Dynamic Multiblock Grids Including Chemical Equilibrium, Volume II," WL-TR-92-7044, Eglin Air Force Base, FL, October 1992.
  4. Mansfield, F. A. and Whitfield, D. L., "Investigation of Solution Operators for the Three-Dimensional Unsteady Euler Equations," AIAA Paper No. 92-2666, June 1992.
  5. Buggeln, R. C., Shamroth, S. J. and Briley, W. R., "Development of a Dynamic Lift Analysis," SRA Report R92-920043-F, NASA Contract N00019-91-C-0088, 1992.
  6. Simpson, L. B. and Whitfield, D. L., "Flux-Difference Split Algorithm for Unsteady Thin-Layer Navier-Stokes Solutions," AIAA Journal, Vol. 30, No. 4, April 1992, pp. 914-922.
  7. Janus, J. M., Horstman, H. Z., and Whitfield, D. L., "Unsteady Flowfield Simulation of Ducted Prop-Fan Configurations," AIAA Paper No. 92-0521, January 1992.
  8. Mansfield, F. A. and Whitfield, D. L., "Investigation of Solution Operators for the Two-Dimensional Unsteady Euler Equations," AIAA Paper No. 92-0050, January 1992.
  9. Janus, J.M., Cox, C.F., Arabshahi, A., Cinnella, P., and Whitfield, D.L., "Numerical Solution and Algorithm Analysis for the Unsteady Navier-Stokes Equations on Dynamic Multiblock Grids Including Chemical Equilibrium," Vol. 2, Report No. WL-TR-92-7044, Wright Laboratory, 1992.
  10. 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.
  11. 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.
  12. 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, (Mar-Apr 1992), p. 247-252.
  13. Liu, N.S., Shamroth, S.J., McDonald, H., “Reciprocal interactions of hairpin-shaped vortices and a boundary layer,” AIAA Journal, vol. 29, (May 1992), p. 720-727.
  14. 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).
  15. Swafford, Timothy W., Huddleston, David H., Busby, Judy A., and Chesser, B. Lawrence, “Computation of Steady and Unsteady Quasi-One-Dimensional Viscous-Inviscid Interacting Internal Flows at Subsonic, Transonic, and Supersonic Mach Numbers,” Mississippi State University, Engineering and Industrial Research Station ReportMSSU-EIRS-ERC-92-1, June 1992.
  16. Reddy, T.S.R., Bakhle, Milind A., Huff, D.L., and Swafford, T.W., “Analysis of Cascades Using a Two Dimensional Euler Solver,” AIAA-92-2370, April 1992.

1991 (back to top)

  1. Taylor, L. K. and Whitfield, D. L., "Unsteady Three-Dimensional Incompressible Euler and Navier-Stokes Solver for Stationary and Dynamic Grids," AIAA Paper No. 91-1650, June 1991.
  2. Whitfield, D. L. and Taylor, L. K., "Discretized Newton-Relaxation Solution of High Resolution Flux-Difference Split Schemes," AIAA Paper No. 91-1539, June 1991.
  3. Govindan, T. R., Briley, W. R., and McDonald, H., "General Three-Dimensional Viscous Primary/Secondary Flow Analysis," AIAA Journal, Vol. 29, No. 3, pp. 361-390, 1991.
  4. 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.
  5. Govindan, T. R. and Briley, W. R., "Generalized Primary/Secondary Flow Analysis of Viscous Flow Around Bodies at Incidence," AIAA Paper No. 91-0186 (29th Aerospace Sciences Meeting, Reno, NV), 1991.
  6. Arabshahi, A. and Whitfield, D. L., “Numerical Simulation of Supersonic Unsteady Flow for Multibody Configuration,” AIAA-91-0023, AIAA 29th Aerospace Sciences Meeting and Exhibit, Reno, NV, January 1991.
  7. 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. 215-224, 1991.
  8. Reddy, T.S.R., Bakhle, Milind A., Huff, D.L., and Swafford, T.W., “Flutter Analysis of Cascades Using a Two Dimensional Euler Solver,” AIAA-91-1681, June 1991.
  9. Huff, D.L., Swafford, T.W., and Reddy, T.S.R., “Euler Flow Predictions for An Oscillating Cascade Using a High Resolution Wave-Split Scheme,” ASME-91-GT-198, June 1991.
  10. Swafford, T.W., Unsteady Viscous-Inviscid Interaction via Direct Coupling of the 1D Euler and 2D Integral Boundary-Layer Equations,” Mississippi State University, Engineering and Industrial Research Station ReportMSSU-EIRS-ERC-90-1, March 1991.
  11. Karman, Jr., S.L., Spragle, G.S., “Development of an Unstructured CFD Method,” AIAA 91-0019, 1991.
  12. Karman, Jr., S.L., “Development of a 3D Unstructured CFD Method,” Ph.D. Dissertation, May 1991, University of Texas at Arlington.
  13. Karman, Jr., S.L., Spragle, G.S., “Calibration of 2D Unstructured Grid Methods on Propulsive Flowfields,” AGARD Fluid Dynamics Panel Symposium on “Aerodynamic Engine-Airframe Integration,” Paper No. 27, October, 1991.
  14. Melnik, R. E., "Some Applications of Asymptotic Theory to Turbulent Flow," presented at the 29th Aerospace Sciences Meeting, Reno, Nevada, AIAA Paper No. 91-0220, January,1991.
  15. Melnik, R. E., "Navier-Stokes 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)

  1. Whitfield, D. L., "Newton-Relaxation Schemes for Nonlinear Hyperbolic Systems," Engineering & Industrial Research Station Report, MSSU-EIRS-ASE-90-3, Mississippi State University, Mississippi State, MS, October 1990.
  2. 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. 90-3093, August 1990.
  3. Liu, N. -S., Davoudzadeh, F., Briley, W. R. and Shamroth, S. J., "Navier-Stokes Simulation of Transonic Blade-Vortex Interactions," Journal of Fluids Engineering, Vol. 112, pp. 501-509, 1990.
  4. Briley, W. R., Govindan, T. R. and McDonald, H, "Efficient Navier Stokes Flow Prediction Algorithms," SRA Report R90 900068 F, 1990.
  5. DeJong, F.J., Sabnis, J.S., Buggeln, R.C., McDonald, H., “Hypersonic Flow Calculations with a Hybrid Navier-Stokes/Monte Carlo Method,” AIAA paper 90-1691. AIAA/ASME 5th Thermophysics and Heat Transfer Conference, Seattle, WA, June 1990, p. 15.
  6. Liu, N.S., Shamroth, S.J., McDonald, H., “Reciprocal Interactions of Hairpin-Shaped Vortices and a Boundary Layer,” AIAA Paper No. 90-0017, AIAA, 28th Aerospace Sciences Meeting, Reno, NV, January 1990, p. 11.
  7. Govindan, T.R., DeJong, F.J., Briley, W.R., McDonald, H., “Rotating Flow in Radial Turbomachinery," Scientific Research Associates, Report No. AD-A222885; SRA-R930011-F; ARO-22360.4-EG-S, May 1990.

1989 (back to top)

  1. Arabshahi, A. and Whitfield, D. L., "A Multiblock Approach to Solving the Three-Dimensional Unsteady Euler Equations About A Wing-Pylon-Store Configuration," AIAA Paper No. 89-3401, Presented at the AIAA Atmospheric Flight Mechanics Conference, Boston, MA, August 14-16, 1989.
  2. Simpson, L. B. and Whitfield, D. L., "A Flux-Difference Split Algorithm for Unsteady Thin-Layer Navier-Stokes Solutions," AIAA Paper No. 89-1995, June 1989.
  3. Whitfield, D. L. and Thompson, J. F., "Computation of Transonic Flow About Stores," AFATL-TR-89-20, Eglin Air Force Base, FL, June 1989.
  4. 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 Three-Dimensional Configurations, Leon, Norway, May 24-25, 1989.
  5. Janus, J. M. and Whitfield, D. L., "A Simple Time-Accurate Turbomachinery Algorithm with Numerical Solutions of an Uneven Blade Count Configuration," AIAA Paper No. 89-0206, January 1989.
  6. Whitfield, D. L., Janus, M. J., and Arabshahi, A., “Unsteady Euler Solutions on Dynamic Grids for Complex Configurations,” AGARD-CP-464, Loen, Norway, May 1989.
  7. Arabshahi, A., “A Dynamic Multiblock Approach to Solving the Unsteady Euler Equations about Complex Configurations,” Ph.D. Dissertation, May 1989.
  8. Razzaghi, M. and Arabshahi, A., “Solutions of Linear Two-Point Boundary Value Problems Via Polynomial Series,”International Journal of Systems Science, Vol. 20, No. 3, pp. 375-384, 1989.
  9. Razzaghi, M., Tahai, A., and Arabshahi, A., “Solutions of Two-Point Boundary Value Problems via Fourier Series and Application to Optimal Control of Linear Systems,” Journal of Franklin Institute, Vol. 326, No. 4, pp. 523-533, 1989.
  10. 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. 1141-1148, 1989.
  11. Razzaghi, M. and Arabshahi, A., “Analysis of Linear Time-Varying Systems and Bilinear Systems Via Fourier Series,” International Journal of Control, Vol. 50, No. 3, pp. 889-898, 1989.
  12. Sabnis, J.S., Gibeling, H.J., McDonald, H., “Navier-Stokes analysis of solid propellant rocket motor internal flows,”Journal of Propulsion and Power, Vol. 5, (Nov-Dec 1989), pp. 657-664.
  13. 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. 30-1 to 30-22
  14. Sabnis, J.S., Madabhushi, R.K., Gibeling, H.J., McDonald, H., “On the Use of k-Epsilon Turbulence Model for Computation of Solid Rocket Internal Flows,” AIAA Paper No. 89-2558, AIAA/ASME/SAE/ASEE 25th Joint Propulsion Conference, Monterey, CA, July 1989, p. 12.
  15. Briley, W.R., Buggeln, R.C., McDonald, H., “Solution of the Incompressible Navier-Stokes Equations Using Artificial Compressibility Methods.” Proceedings of the 11th International Conference on Numerical Methods in Fluid Dynamics, Berlin and New York, Springer-Verlag, 1989, pp. 156-160.
  16. 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.
  17. Melnik, R. E., "An Asymptotic Theory of Turbulent of Turbulent Separation," Computers and Fluids, Vol.17, 1989

1988 (back to top)

  1. Anderson, W. K., Thomas, J. L., and Whitfield, D. L., "Three-Dimensional Multigrid Algorithms for the Flux-Split Euler Equations," NASA-TP-2829, November 1988.
  2. Mounts, J. S., Belk, D. M., and Whitfield, D. L., "Program EAGLE User's Manual: Vol. IV - Multiblock Implicit, Steady-State Euler Code," AFATL-TR-88-117, Vol. IV, Air Force Armament Laboratory, September 1988.
  3. 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.
  4. Thompson, J. F. and Whitfield, D. L., "Transonic Flow Solutions on General 3D Regions Using Composite-Block Grids," 11th International Conference on Numerical Methods in Fluid Dynamics, Williamsburg, VA, June 27 - July 1, 1988.
  5. Anderson, W. K., Thomas, J. L., and Whitfield, D. L., "Multigrid Acceleration of the Flux-Split Euler Equations,"AIAA Journal, Vol. 26, No. 6, June 1988, pp. 649-654.
  6. Janus, J. M. and Whitfield, D. L., "Improved 3-D Turbomachinery CFD Algorithm," Final Report, Prepared for Scientific Research Associates, Inc., Glastonbury, CT, June 1988.
  7. Pirzadeh, S. and Whitfield, D. L., "Three-Dimensional Unsteady Transonic Viscous-Inviscid Interaction Using the Euler and Boundary-Layer Equations," AIAA Paper No. 88-2578, June 1988.
  8. Govindan, T. R., Briley, W. R. and Levy, R., "Computation of Flow Around Maneuvering Submerged Bodies. SRA Report R88 920029 F, 1988.
  9. Whitfield, D. L., Janus, J. M., and Simpson, L. B., "Implicit Finite Volume High Resolution Wave-Split Scheme for Solving the Unsteady Three-Dimensional Euler and Navier-Stokes Equations on Stationary or Dynamic Grids,"Engineering and Industrial Research Station Report MSSU-EIRS-ASE-88-2, Mississippi State University, Mississippi State, MS, February 1988.
  10. 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.
  11. Liu, N.S., Shamroth, S.J., McDonald, H., “Reciprocal interactions of Hairpin-Shaped Vortices and a Boundary Layer,” Scientific Research Associates, Inc., Final Report, February 1, 1986 – December 31, 1988.
  12. Liu, N.S., Shamroth, S.J., McDonald, H., “Flow Dynamics Stimulation by Hairpin-Like Vortices in Initially Laminar Boundary Layers.” Published in Scientific Research Associates, Inc., Annual Report, March 1988.

1987 (back to top)

  1. Belk, D. M., Janus, J. M., and Whitfield, D. L., "Three-Dimensional Unsteady Euler Equations Solution on Dynamic Grids," AIAA Journal, Vol. 25, No. 9, September 1987, pp. 1160-1161.
  2. 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," AIAA-87-2614-CP, 5th AIAA Applied Aerodynamics Conference, Monterey, CA, August 1987.
  3. Belk, D. M. and Whitfield, D. L., "Time-Accurate Euler Equations Solutions on Dynamic Blocked Grids," AIAA Paper No. 87-1127-CP, June 1987.
  4. Gatlin, B. and Whitfield, D. L., "An Implicit Upwind Finite Volume Method for Solving the Three-Dimensional Thin-Layer Navier-Stokes Equations," AIAA Paper No. 87-1149-CP, June 1987.
  5. Whitfield, D. L., Swafford, T. W., Janus, J. M., Mulac, R.A., and Belk, D. M., "Three-Dimensional Unsteady Euler Solutions for Propfans and Counter-Rotating Propfans in Transonic Flow," AIAA Paper No. 87-1197, June 1987.
  6. Belk, D. M. and Whitfield, D. L., "3-D Euler Solutions on Blocked Grids Using an Implicit Two-Pass Algorithm," AIAA Paper No. 87-0450, January 1987.
  7. Govindan, T.R., McDonald, H., “Computation of Tip and Corner Region Flows.” AGARD Computation of Three-Dimensional Boundary Layers Including Separation, February 1987, p. 20.
  8. Sabnis, J.S., Gibeling, H.J., McDonald, H., “Navier-Stokes Analysis of Two- and Three-Dimensional Flow Field in Solid Rocket Motors with Segment Joints.” AIAA/SAE/ASME/ASEE, 23rd Joint Propulsion Conference, San Diego, CA, July 1987, p. 11.
  9. Sabnis, J.S., Gibeling, H.J., McDonald, H., “A Combined Eulerian-Lagrangian Analysis for Computation of Two-Phase Flows.” AIAA Paper 87-1419, AIAA 19th Fluid Dynamics, and Lasers Conference, Honolulu, HI, June 1987, p. 10.
  10. Buggeln, R. C., Briley, W.R., McDonald, H., Shamroth, S.J., Weinberg, B.C., “Two- and Three-Dimensional 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. 199-209.
  11. 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.
  12. Chan, Y.T., Buggeln, R.C., McDonald, H., “Three-Dimensional Dynamic Labyrinth Seal Analysis,” Published in Scientific Research Associates, Inc., Final Report, January 1987, p. 50.
  13. Liu, N.S., Shamroth, S.J., McDonald, H., “Flow Dynamics Stimulated by Hairpin-Like Vortices in Initially Laminar Boundary Layers.” Published in Scientific Research Associates, Inc., Annual Report, February 1987, p. 22.
  14. 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, co-authors, February, 1987.
  15. Melnik, R. E., "A New Asymptotic Theory of Turbulent Boundary Layers and Its Application to Separation," Boundary Layer Separation, Springer Verlag, New York,1987.
  16. Melnik, R. E., "An Overview of Computational Fluid Dynamics Development and Application at Grumman," presented at the NASA Conference on Supercomputing in Aerospace, 10-12 March 1987.

1986 (back to top)

  1. Janus, J. M. and Whitfield, D. L., "Advanced 3-D Viscous SSME Turbine Rotor Stator CFD Algorithms," Final Report NAS8-36486, Prepared for George C. Marshall Space Flight Center, Marshall Space Flight Center, Alabama, September 1986.
  2. 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.
  3. Briley, W. R. and McDonald, H., "Accuracy and Iterative Convergence Rate of ADI Schemes for Scalar Convection," SRA Report R86 900050 F, 1986.
  4. Belk, D. M., Janus, J. M., and Whitfield, D. L., "Three-Dimensional Unsteady Euler Equations Solutions on Dynamic Grids," AFATL-TR-86-21, Air Force Armament Laboratory, April 1986.
  5. Anderson, W. K., Thomas, J. L., and Whitfield, D. L., "Multigrid Acceleration of the Flux Split Euler Equations," AIAA Paper No. 86-0274, January 1986.
  6. Kim, Y.N., Buggeln, R.C., McDonald, H., “Numerical Analysis of Some Supersonic Viscous Flows Related to Inlet and Nozzle Systems.” AIAA Paper 86-1597, AIAA/ASME/SAE/ASEE 22nd Joint Propulsion Conference, Huntsville, AL, June 1986, p. 13.
  7. 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.
  8. 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.
  9. 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. 233-235.
  10. Briley, W.R., Govindan, T.R., Levy, R., McDonald, H., “Numerical Study of Three-Dimensional Laminar and Turbulent Flows with System Rotation.” Published in Scientific Research Associates, Inc., Final Report, 1986, p. 46.
  11. 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.
  12. Buggeln, R.C., Kim, Y.N., McDonald, H., “Computation of Multi-Ddimensional Viscous Supersonic Flow,” Published in Scientific Research Associates, Inc., Final Report, (Oct. 1986), p. 194.
  13. Kim, Y.N, Buggeln, R.C., McDonald, H., “Computation of Multi-Dimensional Viscous Supersonic Jet Flow,” Published in Scientific Research Associates, Inc., Final Report (Oct 1986), p. 128.
  14. Weinberg, B.C., McDonald, H., “Influence of Large-Scale Motion on Turbulent Transport for Confined Coaxial Jets. Volume 2: Navier-Stokes Calculation of Swirling and Nonswirling Confined Coaxial Jets,” Published in Scientific Research Associates, Inc., Final Report, January 1986, p. 57.
  15. Buggeln, R.C., Briley, W.R., McDonald, H., “Solution of the Three-Dimensional Navier Stokes Equations for a Turbulent Horseshoe Vortex Flow,” Published in Scientific Research Associates, Inc. Final Report, October 1985 – September 1986, p. 36.
  16. Briley, W.R. and McDonald, H., "Accuracy and Iterative Convergence Rate of ADI Schemes for Scalar Convection," SRA Report R86 900050 F, 1986.
  17. Phares, W.J., Cooper, G.K., Swafford, T.W., and Jones, R.R., “Application of Computational Fluid Dynamics to Test Facility and Experiment Design,” AIAA-86-1733, June 1986.
  18. Karman, Jr., S.L., Steinbrenner, J.P., Kisielewski, K.M., “Analysis of the F-16 Flow Field by a Block Grid Euler Approach,” AGARD-CP-412 Paper No. 18, Published November, 1986.
  19. Reed, C.L., Karman, Jr., S.L., “Multiple-Block Grid Method Applied to Complex 3-D Geometries,” Presented at Society for Industrial and Applied Mathematics 1986 National Meeting, July 1986, Boston, Mass. Unpublished.
  20. 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, 23-25 June 1986, published in Lecture Notes in Physics, 264, Springer Verlag, 1986 (coauthor).

1985 (back to top)

  1. 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.
  2. 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.
  3. Whitfield, D. L., "Implicit Upwind Finite Volume Scheme for the Three Dimensional Euler Equations," Engineering and Industrial Research Station Report MSSU-EIRS-ASE-85-1, Mississippi State University, Mississippi State, MS, September 1985.
  4. Belk, D. M., Janus, J. M., and Whitfield, D. L., "Three-Dimensional Unsteady Euler Equations Solutions on Dynamic Grids," AIAA Paper No. 85-1704, July 1985.
  5. Swafford, T. W. and Whitfield, D. L., "Time-Dependent Solution of Three-Dimensional Compressible Turbulent Integral Boundary-Layer Equations," AIAA Journal, Vol. 23, No. 7, July 1985, pp. 1005-1013.
  6. Whitfield, D. L., "Viscous-Inviscid Interaction Computations Using a Pseudo Navier-Stokes Approach," inNumerical and Physical Aspects of Aerodynamic Flows III, T. Cebeci, Editor, Springer-Verlag, New York, 1985.
  7. Whitfield, D. L. and Thomas, J. L., "Transonic Viscous-Inviscid Interaction Using Euler and Inverse Boundary-Layer 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.
  8. 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. 84-1520 CP, 7th CFD Conference (Univ. Cincinnati), 1985.
  9. Lin, S. J., Briley, W. R. and McDonald, H., "Numerical Study of Three Dimensional Viscous Flows With System Rotation," AIAA Paper No. 85-1691 CP, (18th Fluid Dynamics and Plasmadynamics and Lasers Conference, Cincinnati OH), 1985.
  10. Briley, W. R., McDonald, H. and Buggeln, R. C., "Observations on Three Dimensional Viscous Turbine Flow Analysis Methods," SRA Report R85 900029 F, 1985.
  11. 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. 2.1-2.6.
  12. Weinberg, B.C., Yang, R.J., McDonald, H., Shamroth, S.J., “Calculations of Two and Three-Dimensional Transonic Cascade Flow Fields Using the Navier-Stokes Equation,” ASME paper 85-GT-66, ASME 30th International Gas Turbine Conference and Exhibit, Houston, TX, March 1985, p. 10.
  13. Roscoe, D.V., Gibeling, H.J., McDonald, H., Shamroth, S.J., “Development of a Navier-Stokes 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. 4-15 – 4-23.
  14. Briley, W.R., Buggeln, R.C., McDonald, H., “Solution of the Three-Dimensional Navier-Stokes Equations for a Steady Laminar Horseshoe Vortex Flow.” Proceedings of the AIAA 7th Computational Fluid Dynamics Conference, Cincinnati, OH, July 1985, pp. 299-312.
  15. Lin, S.J., Briley, W.R., McDonald, H., “Numerical Study of Three-Dimensional Viscous Flows with System Rotation.” AIAA 18th Fluid Dynamics and Plasmadynamics and Lasers Conference, Cincinnati, OH, July 1985, p. 13.
  16. Sabnis J.S., Gibeling, H.J., McDonald, H., “Calculation of Solid Propellant Rocket Motor Internal Flow Field Using an Implicit Navier-Stokes Procedure.” AIAA 18th Fluid Dynamics and Plasmadynamics and Lasers Conference, Cincinnati, OH, July 1985, p. 7.
  17. Weinberg, B.C., McDonald, H., Shamroth, S.J., “A Solution Procedure for Two- and Three-Dimensional Unsteady Viscous Flows.” AIAA 23rd Aerospace Sciences Meeting, Reno, NV, Jan. 1985, p. 15.
  18. Yang, R.J., Weinberg, B.C., Shamroth, S.J., McDonald, H., “Numerical Solutions of the Navier-Stokes Equations for Two- and Three-Dimensional Turbine Cascades with Heat Transfer,” Published in General Motors Corp, Final Report, July 1985, p. 160.
  19. Lui, N.S., Shamroth, S.J., McDonald, H., “Numerical Simulation of Unsteady Three-Dimensional Turbulent Structures in Boundary Layer Flow,” Published in Scientific Research Associates, Inc., Final Report, November 1984 – May 1985, p. 45.
  20. Kim, Y.N., Buggeln, R.C., McDonald H., “Development of a Navier-Stokes Analysis for the Flow in Disk Pumps,” Published in Scientific Research Associates, Inc. Final Report, September 1984 – March 1985, p. 45.
  21. Swafford, T.W., “Time-Dependent Inverse Solution of Three-Dimensional Compressible, Turbulent Integral Boundary-Layer Equations in Non-orthogonal Curvilinear Coordinates,” Lecture Notes in Physics, Vol. 218, Springer-Verlag, 1985, pp. 541-545.
  22. 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, 21-24 January 1985.
  23. Melnik, R. E., "Similarity Solutions for Plane and Radial Jets Using a k-e Turbulence Model," Trans. ASMC Journal ed Fluids Engineering, Vol. 107, No. 1 March 12, 1985, (coauthor).
  24. Melnik, R. E., "A Method for Design of Closed Airfoils for Arbitrary Supercritical Speed Distributions," AIAA paper No. 85-5023, AIAA 3rd Applied Aerodynamics Conference, 14-16 October 1985, (coauthor).
  25. Melnik, R. E., "An Improved Viscid/Inviscid Interaction Procedure for Transonic Flow Over Airfoils," NASA Contract Report 3805, October 1985, (coauthor).
  26. 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)

  1. Whitfield, D. L. and Jameson, A., "Euler Equation Simulation of Propeller-Wing Interaction in Transonic Flow,"Journal of Aircraft, Vol. 21, No. 11, November 1984, pp. 835-839.
  2. Whitfield, D. L. and Janus, J. M., "Three-Dimensional Unsteady Euler Equations Solution Using Flux Vector Splitting," AIAA Paper No. 84-1552, June 1984.
  3. Whitfield, D. L., Thomas, J. L., Jameson, A., and Schmidt, W., "Computation of Transonic Viscous-Inviscid Interacting Flow," in Numerical and Physical Aspects of Aerodynamic Flows II, T. Cebeci, Editor, Springer-Verlag, New York, 1984, pp. 285-295.
  4. 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. 374-382, 1984.
  5. Briley, W. R. and McDonald, H., "Three Dimensional Viscous Flows with Large Secondary Velocity," J. Fluid Mechanics, Vol. 144, pp. 47-77, 1984 (coauthor).
  6. 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.383-390, 1984.
  7. 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.
  8. 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.
  9. Arabshahi, A., “Correlations for the Drag Coefficient of Blunt Circular Cylinders in Transonic Axial Flow,” Master’s Thesis, May 1984.
  10. 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): 374-382, 1984.
  11. 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: 383-390, 1984.
  12. 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. 195-205.
  13. Weinberg, B.C., Yang, R.J., Shamroth, S.J., McDonald, H., “Calculation of Two- and Three-Dimensional Transonic Cascade Flow Field Using the Navier-Stokes Equations,” Published by NASA Lewis Research Center’s Turbine Engine Hot Section Technology Report, October 1984, p. 8.
  14. Briley, W. R., Buggeln, R.C., McDonald, H., “Solution of the Three-Dimensional Navier-Stokes Equations for a Steady Laminar Horseshoe Vortex Flow,” Scientific Research Associates, Inc., Final Report, June 1982 – June 1984, p. 43.
  15. Shamroth, S.J., McDonald, H., Weinberg, B.C., Roscoe, D.V., “Development of a Navier-Stokes Rotor and Stator Analysis,” Scientific Research Associates, Inc., Annual Report, June 1984, p. 39.

1983 (back to top)

  1. Swafford, T. W. and Whitfield, D. L., "Numerical Solutions of Three-Dimensional Time-Dependent Compressible Turbulent Integral Boundary-Layer Equations in General Curvilinear Coordinates," AIAA Paper No. 83-1674, July 1983.
  2. 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.
  3. 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. 1467-1469, 1983.
  4. Schmidt, W., Jameson, A., and Whitfield, D., "Finite-Volume Solutions to the Euler Equations in Transonic Flow,"Journal of Aircraft, Vol. 20, No. 2, February 1983, pp. 127-133.
  5. Whitfield, D. L. and Jameson, A., "Three-Dimensional Euler Equation Simulation of Propeller-Wing Interaction in Transonic Flow," AIAA Paper No. 83-0236, January 1983.
  6. Liu, N.S., Shamroth, S.J., McDonald, H., “Numerical Solution of the Navier-Stokes Equations for Compressible Turbulent Two/Three Dimensional Flows in the Terminal Shock Region of an Inlet/Diffuser.” AIAA Paper 83-1892,AIAA 6th Computational Fluid Dynamics Conference, Danvers, MA (Jul. 1983), pp. 61-71. 45.
  7. 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.
  8. 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.
  9. Gibeling, H.J., Briley, W.R., Kreskovsky, J.P., Shamroth, S.J., McDonald, H., “Computation of Discrete Slanted Hole Film Cooling Flow Using the Navier-Stokes Equations,” Scientific Research Associates, Inc., Final Report, September 1983, p. 63.
  10. Lin, S.J., Kreskovsky, J.P., Briley, W.R., McDonald, H., “Further Development of a Method for Computing Three-Dimensional Subsonic Viscous Flows in Turbofan Lobe Mixers,” Scientific Research Associates, Inc., Final Report, November. 1983, p. 66.
  11. Swafford, T.W., “Three-Dimensional, Time-Dependent, Compressible, Turbulent, Integral Boundary-Layer Equations in General Curvilinear Coordinates and Their Numerical Solution,” AEDC-TR-83-37, Arnold AFB, TN, September 1983.
  12. Swafford, T.W., “Analytical Approximation of Two Dimensional Separated Turbulent Boundary Layer Velocity Profiles,” AIAA Journal, Vol. 21, No. 6, June 1983, pp. 923-926.
  13. Swafford, T.W., “Three-Dimensional, Time-Dependent, Compressible, Turbulent, Integral Boundary-Layer Equations in General Curvilinear Coordinates and Their Numerical Solution,” PhD Dissertation, Mississippi State University, August 1983.

1982 (back to top)

  1. 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, Springer-Verlag, Berlin, 1982.
  2. 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.
  3. 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.
  4. Briley, W. R. and McDonald, H., "Computation of Turbulent Horseshoe Vortex Flow Past Swept and Unswept Leading Edges," SRA Report R82 920001 F, 1982.
  5. 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.
  6. 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. 99-120, 1982.
  7. 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.
  8. Kreskovsky, J.P., Briley, W.R., McDonald, H., “Turbofan Forced Mixer-Nozzle Internal Flowfield. Volume 3; A Computer Code for 3-D Mixing in Axisymmetric Nozzles,” Published in Scientific Research Associates, Inc., Final Report, April 1982, Vol. 3, p. 129.

1981 (back to top)

  1. Whitfield, D. L., Swafford, T. W., and Jacocks, J. L., "Calculation of Turbulent Boundary Layers with Separation and Viscous-Inviscid Interaction," AIAA Journal, Vol. 19, No. 10, October 1981, pp. 1315-1322.
  2. 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. 81-1265, June 1981.
  3. Whitfield, D. L., Jameson, A., and Schmidt, W., "Viscid-Inviscid Interaction on Airfoils Using Euler and Inverse Boundary-Layer Equations," Presented at the U.S.-German Data Exchange Meeting at DFVLR-AVA in Gottingen, Germany, April 1981.
  4. Kreskovsky, J.P., Briley, W.R, McDonald, H., “Analysis and Computation of Three-Dimensional Flow in Strongly Curved Ducts.” ASME Winter Annual Meeting, Washington, D.C., November 1981, A82-29001 13-02; American Society of Mechanical Engineers, 1981, pp. 129-140.
  5. Briley, W.R., McDonald, H., “Computation of Three-Dimensional 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, Springer-Verlag, 1981, pp. 91-98.
  6. Buggeln, R.C., Briley, W.R., McDonald, H., “Solution of the Navier-Stokes Equations for Three-Dimensional Turbulent Flow with Viscous Sublayer Resolution.” AIAA paper 81-1023, Proceedings of the AIAA 5th Computational Fluid Dynamics Conference, Palo Alto, CA, June 1981. Collection of Technical Papers, 1981, pp. 247-256.
  7. 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.
  8. Levy, R., McDonald, H., Briley, W.R., Kreskovsky, J.P., “A Three-Dimensional Turbulent Compressible Subsonic Duct Flow Analysis for Use with Constructed Coordinate Systems,” Scientific Research Associates, Inc., Final Report, 1981, p. 40.
  9. 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.
  10. Gibeling, H.J., Kreskovsky, J.P., Briley, W.R., McDonald, H., “Computation of Discrete Hole Film Cooling Flow Using the Navier-Stokes Equations,” Published in Scientific Research Associates, Inc., Annual Report, April 1980 – March 1981, p. 28.

1980 (back to top)

  1. Whitfield, D. L., Swafford, T. W., and Jacocks, J. L., "Calculation of Turbulent Boundary Layers with Separation, Reattachment, and Viscous-Inviscid Interaction," AIAA Paper No. 80-1439, July 1980.
  2. 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. 71-99.
  3. 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.
  4. 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. 91-98.
  5. 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.
  6. 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.
  7. 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.
  8. Shamroth, S.J., Gibeling, H.J., McDonald, H., “A Navier-Stokes 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.
  9. Buggeln, R.C., McDonald, H., Kreskovsky, J.P., Levy, R., “Computation of Three-Dimensional Viscous Supersonic Flow in Inlets.” AIAA Paper 80-0194, AIAA 18th Aerospace Sciences Meeting, Pasadena, CA, January 1980, p. 12.
  10. Buggeln, R.C., McDonald, H., Levy, R., Kreskovsky, J.P., “Development of a Three-Dimensional Supersonic Inlet Flow Analysis,” Scientific Research Associates, Inc., Final Report, January 1980, p. 122.
  11. Swafford, T.W., “Analytical Approximation of Two Dimensional Separated Turbulent Boundary Layer Velocity Profiles,” AEDC-TR-79-99, Arnold AFB, TN, October 1980.
  12. Swafford, T.W., “Computational Support to Tests at AEDC/PWT,” AEDC-TMR-80-P32, Arnold AFB, TN, September 1980 (Limited Distribution).

1979 (back to top)

  1. Whitfield, D. L., "Analytical Description of the Complete Turbulent Boundary Layer Velocity Profile," AIAA Journal, Vol. 17, No. 10, October 1979, pp. 1145-1147.
  2. 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.
  3. 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.
  4. 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.
  5. McDonald, H., “Combustion modeling in two and three dimensions – Some numerical considerations.” Progress in Energy and Combustion Science, Vol 5, No. 2, (1979) pp. 97-122.
  6. 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.
  7. McDonald H., “Computational Aspects of Viscous Flows (Numerical Analysis of Viscous Flow and the Relationship of the Boundary Layer Equations to the Navier-Stokes 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.
  8. Kreskovsky, J.P., Briley, W.R., McDonald, H., “Computation of Discrete Hole Film Cooling Flow Using the Navier-Stokes Equations (Gas Turbine Blades),” Scientific Research Associates, Inc., Final Report, July 1979, p. 17.
  9. Weinberg, B.C., McDonald, H., “Solution of 3-Dimensional Time-Dependent 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 NASA-CR-166565-PT-1, April 1979, p. 86.
  10. Swafford, T.W., Calculation of Skin Friction in Two Dimensional, Transonic, Turbulent Flow,” AEDC-TR-79-12, Arnold AFB, TN, 1979.

1978 (back to top)

  1. Whitfield, D. L., "Integral Solution of Compressible Turbulent Boundary Layers Using Improved Velocity Profiles," AEDC-TR-78-42, August 1978.
  2. Sinclair, D. W., Whitfield, D. L., and Lucci, C. A., "Holographic Interferometry Measurements of Subsonic Turbulent Boundary Layers," AIAA Paper No. 78-119, July 1978.
  3. 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.
  4. Whitfield, D. L., "Analytical Description of the Complete Turbulent Boundary Layer Velocity Profile," AIAA Paper No. 78-1158, 1978.
  5. Levy R., McDonald, H., Briley, W.R., “Calculation of Three-Dimensional Turbulent Subsonic Flow in Transition Ducts,” Proceedings of 6th International Conference on Numerical Methods in Fluid Dynamics, Tiflis, GA, June 1978, pp. 361-369.
  6. Eiseman, P.R., Levy, R., McDonald, H., Briley, W.R., “Development of a Three-Dimensional Turbulent Duct Flow Analysis,” United Technologies Research Center, East Hartford, CT., Final Report, November 1978, p. 117.
  7. Anderson, O. L., Briley, W.R., McDonald H., “Derivation and Evaluation of an Approximate Analysis for Three-Dimensional 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)

  1. Whitfield, D. L., "Analytical Description of the Complete Two-Dimensional Turbulent Boundary-Layer Velocity Profile," AEDC-TR-77-79, September 1977.
  2. Whitfield, D. L., "Turbulent Flow Near a Wall Based on a Turbulent Kinetic Energy Equation," in Boundary Layer Effects-Proceedings of the 5th U.S. Air Force-Federal Republic of Germany Data Exchange Agreement Meeting, A.W. Fiore, Editor, AFFDL-TR-77-61, July 1977, pp. 447-454.
  3. Whitfield, D. L. and High, M. D., "Velocity-Temperature Relations in Turbulent Boundary Layers with Non-Unity Prandtl Numbers," AIAA Journal, Vol. 15, No. 3, March 1977, pp. 431-434.
  4. 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. 372-397.
  5. 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.
  6. 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)

  1. Whitfield, D. L., "Analytical, Numerical and Experimental Results on Turbulent Boundary Layers," AEDC-TR-76-62, July 1976.
  2. Whitfield, D. L. and High, M. D., "Velocity-Temperature Relations in Turbulent Boundary Layers with Non-Unity Prandtl Numbers," AIAA Paper No. 76-411, July 1976.
  3. Whitfield, D. L., "Infrared Turbojet Plume Radiation," AEDC-TR-76-14, February 1976.
  4. Hall, G.F., Shamroth, S.J., McDonald, H., Briley, W.R., “The Inviscid Pressure Field on the Tip of a Semi-Infinite Wing and Its Application to the Formation of a Tip Vortex,” United Technologies Research Center, East Hartford, CT, Final Report, October 1976, p. 84.
  5. Gibeling, H.J., McDonald, H., “Development of a Three-Dimensional Combustor Flow Analysis. Volume 2: Theoretical Studies,” United Technologies Research Center, East Hartford, CT., Final Report, June 1975 – October 1976, p. 61.
  6. 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.
  7. 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)

  1. Whitfield, D. L., Bertrand, W. T., and Brewer, L. E., "Infrared Radiation Approximation for Homogeneous Plumes," AIAA Paper No. 75-703, May 1975.
  2. 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. 150-178.
  3. Briley, W. R. and McDonald, H., "Numerical Prediction of Incompressible Separation Bubbles," Journal of Fluid Mechanics, Vol. 69, Part 4, 1975, pp. 631-656.
  4. 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.
  5. Shamroth, S.J., McDonald, H., “Application of a Transitional Boundary-Layer in the Low Hypersonic Mach Number Regime,” International Journal of Heat and Mass Transfer, Vol. 18, Nov. 1975, pp. 1277-1284.
  6. 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 75-FE-16, ASME, Joint Fluids Engineering and Lubrication Conference, Minneapolis, MN, May, 1975, p. 12.
  7. Briley, W. R., McDonald, H., Gibeling, H.J., “Solution of the Multidimensional Compressible Navier-Stokes 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)

  1. Whitfield, D. L., "Some Computations of Turbulent Boundary Layers," ARO- ER-74-3, August 1974.
  2. Whitfield, D. L., "Some Improvements in Data Reduction of Pitot Pressure Measurements in Turbulent Boundary Layers," ARO-ER-74-4, August 1974.
  3. 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. 870-872.
  4. Whitfield, D. L., "Heat Flux to Normal Flat Plates in Rarefied Hypersonic Flow," Rarefied Gas Dynamics, Vol. II, DFVLR-Press, Porz-Wahn, German, 1974, pp. D.18.1-D.18.7.
  5. Briley, W.R., "A Numerical Method for Predicting Three Dimensional Viscous Flows in Ducts," Journal of Computational Physics, Vol. 14, No. 1, 1974, pp. 8-28.
  6. 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.
  7. 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. 705-716.
  8. 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.
  9. 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)

  1. Whitfield, D. L., "Mean Free Path of Emitted Molecules and Correlation of Sphere Drag Data," AIAA Journal, Vol. 11, No. 12, December 1973, pp. 1666-1670.
  2. 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. 1336-1337.
  3. 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. 73-642, July 1973.
  4. Whitfield, D. L., "Viscous Effects in Low-Density Nozzle Flows," AEDC-TR-73-52, June 1973.
  5. 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," AEDC-TR-73-11, May 1973.
  6. Whitfield, D. L., "Calibration of a Heat Flux Sensor in Rarefied Hypersonic Flow," LTR-AEDC-VKF-ASP-3-73, March 1973.
  7. Whitfield, D. L., "Rarefied Flow Heat-Flux Calibration of an Earth Satellite Temperature Alarm System," LTR-AEDC-VKF-ASP-1-73, March 1973.
  8. 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.
  9. Whitfield, D. L., "Mean Free Path of Molecules from a Surface in Rarefied Flow with Application to Correlating Drag Data," AIAA Paper No. 73-198, January 1973.
  10. McDonald, H., Fish, R.W., “Practical Calculations of Transitional Boundary Layers,” International Journal of Heat and Mass Transfer, Vol. 16, Sept. 1973, pp. 1729-1744.
  11. 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.
  12. 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.
  13. Briley, W.R., McDonald, H., “An Implicit Numerical Method for the Multidimensional Compressible Navier-Stokes Equations (Application to Three Dimensional Subsonic Flow),” United Technologies Research Center, East Hartford, CT. Report, November 1973, p. 56.

1972 (back to top)

  1. Shamroth, S.J., McDonald, H., “Application of a Time-Independent Boundary-Layer Analysis to the Problem of Dynamic Stall.” ASME, Transactions Journal of Applied Mechanics, Vol. 39, Sept. 1972, pp. 823-825.
  2. Shamroth, S.J., McDonald, H., “A New Solution of the Turbulent Near-Wake Recompression Problem. (Crocco-Lee 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. 121-130.
  3. McDonald, H., Fish, R. W., “Practical Calculations of Transitional Boundary Layers (Finite Difference Procedure for Computing Behavior of Two-Dimensional Boundary Layers and Turbulence Model to Predict Location and Extent of Transition Region,” Published in AGARD Boundary Layer Effects in Turbomachines, December 1972, pp. 29-53.
  4. 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)

  1. Whitfield, D. L., "Drag on Bodies in Rarefied High-Speed Flow," PhD Dissertation, University of Tennessee, December 1971.
  2. 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. 1131-1137.
  3. 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," AEDC-TR-71-135, September 1971.
  4. Smithson, H. K., Price, L. L., and Whitfield, D. L., "Wind Tunnel Testing of Interactions of High Altitude Rocket Plumes with the Free Stream," AEDC-TR-71-118, September 1971.
  5. Whitfield, D. L. and Smithson, H .K., "Low-Density Supersonic Sphere Drag with Variable Wall Temperature," AEDC-TR-71-83, July 1971.
  6. 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)
  7. Whitfield, D. L., "Analysis of Sphere and Cylinder Drag in Rarefied Flow," Rarefied Gas Dynamics, Vol. I., Editrice Tecnico Scientifica, Pisa, Italy, 1971, pp. 527-534.
  8. Briley, W. R., "A Numerical Study of Laminar Separation Bubbles Using the Navier Stokes Equations," Journal of Fluid Mechanics, Vol. 47, Part 4, pp. 713-736, 1971.
  9. 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.).
  10. 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. 377-384.
  11. 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. 1131-1137.
  12. McDonald, H., Shamroth, S.J., “An Analysis and Application of the Time-Dependent Turbulent Boundary-Layer 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. 1553-1560.

1970 (back to top)

  1. Benek, J. A. and Whitfield, D. L., "AFRPL Scarfed Nozzle Condensation Study in 4x6 Research Chamber," LTR-AEDC-VKF-ASP-1-70, December 1970.
  2. Whitfield, D. L., "Dynamics of Particles in Free Molecular Flow with Application to High Altitude Meteoric Dust Collection Devices," AEDC-TR-70-139, August 1970.
  3. Whitfield, D. L. and Lewis, C. H., "Boundary-Layer Analysis of Low-Density Nozzles Including Displacement, Slip, and Transverse Curvature," Journal of Spacecraft and Rockets, Vol. 7, No. 4, April 1970, pp. 462-468.
  4. Whitfield, D. L. and Stephenson, W. B., "Sphere Drag in the Free-Molecular and Transitional Flow Regimes," AEDC-TR-70-32, April 1970.
  5. Stephenson, W. B. and Whitfield, D. L., "Drag Measurements in a Low Density Gas Stream," AEDC-TR-70-25, May 1970.
  6. McDonald, H., “A New Solution of the Turbulent Near-Wake Recompression Problem (Two Dimensional Supersonic Turbulent Near Wake Saddle Point Singularity During Recompression Analyzed by Including Transverse Momentum Integral Equation,” AIAA Paper 70-228, AIAA 8th Aerospace Sciences Meeting, New York, N.Y., January 1970, p. 12.

1969 (back to top)

  1. 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," AEDC-TR-69-196, November 1969.
  2. Whitfield, D. L. and Lewis, C. H., "Analysis of Boundary Layers in Low Density Hypersonic Axisymmetric Nozzles, Including the Effects of Displacement, First-Order Transverse Curvature, Velocity Slip, and Temperature Jump," AIAA Paper No. 69-653, June 1969.
  3. 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. 1449-1453.
  4. McDonald H., “Linear Stress Distribution and the Turbulent Boundary-Layer Equations of Motion,” Physics of Fluids, Vol. 12, Nov. 1969, pp. 2241-2247.
  5. 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. 311-336.

1968 (back to top)

  1. Whitfield, D. L., "Theoretical and Experimental Investigation of Boundary Layers in Low Density Hypersonic Axisymmetric Nozzles," AEDC-TR-68-193, September 1968. (Also MS Thesis, University of Tennessee, June 1968.)
  2. Briley, W.R., "Time Dependent Rotating Flow in a Cylindrical Container," PhD Dissertation, The University of Texas at Austin, August 1968.
  3. McDonald, H., “The Departure from Equilibrium of Turbulent Boundary Layers,” Aeronautical Quarterly, Vol. 19, Feb. 1968, pp. 1-19.
  4. Maise, G., McDonald, H., “Mixing Length and Kinematic Eddy Viscosity in a Compressible Boundary Layer,” AIAA Journal, Vol. 6, Jan. 1968, pp. 73-80.
  5. 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. 83-98.

1967 (back to top)

  1. 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)

  1. McDonald, H., “Turbulent Shear Layer Re-attachment With Special Emphasis on the Base Pressure Problem,”Aeronautical Quarterly, Vol. 15, Aug. 1964, pp. 247-280.
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