Computational Fluid Dynamics

  • Hall, L.H., Applebaum, M.P., Eppard, W.M., Purinton, D.C., “Modeling and Simulation Techniques for the NASA SLS Service Module Panel Separation Event; From Loosely-Coupled Euler to Fully-Coupled 6-DOF, Time-Accurate, Navier-Stokes”, AIAA 2019-1843, SciTech Forum, San Diego, Ca, Jan 7-11, 2019
  • Applebaum, M.P., Hall, L.H., Eppard, W.M., Purinton, D.C., Campbell, J.R., Blevins, J.A., “Development of an Aerodynamic Analysis Method and Database for the SLS Service Module Panel Jettison Event Utilizing Inviscid CFD and MATLAB”, 53rd AIAA Aerospace Sciences Meeting, Kissimmee, Fl, Jan 5-9, 2015
  • Coirier, W. J., Brown, M., Hall, Z., McDaniel, M., “A Pressure Disk Model for Modeling Installed Propeller Performance and Effects on Unmanned Aircraft Systems”, AIAA 2014-2276, Atlanta, GA, 2014.
  • Time-Accurate Simulations of a Spinning Propeller Using OVERFLOW2 (AIAA 2014-3131), William S. Westmoreland, Melissa A. McDaniel, Zachary M. Hall, 32nd AIAA Applied Aerodynamics Conference, 2014, 10.2514/6.2014-3131
  • Brown, M. R., “Numerical Studies of Supersonic Jet Impingement on a Flat Plate”, Ph.D. Dissertation, University of Alabama in Huntsville, Huntsville, AL, 2012.
  • Brown, M. R and Frendi, A., “Supersonic Jet Impingement on a Flat Plate”, AIAA 2012-2261, Colorado Springs, CO, 2012.
  • Applebaum, M.P., Eppard, W.M., Hall, L.H., “Multispecies Effects for Plume Modeling on Launch Vehicle Systems”, Journal of Spacecraft and Rockets, Vol. 49, No. 5 (2012), pp. 770-778
  • Applebaum, M.P., Eppard, W.M., Hall, L.H., Blevins, J., “Protuberance Aerodynamic Loads for Space Launch Systems Using Computational Fluid Dynamics”, Journal of Spacecraft and Rockets, Vol. 49, No. 5 (2012), pp. 779-787.
  • Coirier, William J., Westmoreland, Shawn, Jordan, Keith, Barber, Jennie, Tramel, Robert and Lackey, Shane, “Computational Modeling of a Modified Rod in Cross-Flow Device on a Realistic Fighter Configuration”, AIAA Paper 2011-1220, Orlando, FL, January 2011.
  • Applebaum, M.P., Eppard, W.M., Hall, L.H., Blevins, J., ” Protuberance Aerodynamic Loads for Space Launch Vehicle Systems using CFD”, AIAA 2011-3649, 29th AIAA Applied Aerodynamics Conference, Honolulu, HI, June 27-30, 2011.
  • Hall, L.H., Applebaum, M.P., Eppard, W.M., ” Multi-Species Effects for Plume Modeling on Launch Vehicle Systems”, 49th AIAA Aerospace Sciences Meeting, Orlando, Fl, Jan 4-7, 2011.
  • Hall, L.H., Applebaum, M.P., Eppard, W.M.,” Debris Transport Modeling Techniques on Launch Vehicle Systems”,49th AIAA Aerospace Sciences Meeting, Orlando, Fl, Jan 4-7, 2011.
  • Hall, L.H., Eppard, W.M., Applebaum, M.P., Blevins, J., “Cartesian Euler Code Application for Launch Vehicle Systems”,49th AIAA Aerospace Sciences Meeting, Orlando, Fl, Jan 4-7, 2011.
  • Westmoreland, W. Shawn, “Trajectory Variation Due to an Unsteady Flow-Field”, AIAA Paper 2009-0550 (invited), AIAA ASM, Orlando, FL, January 2009.
  • Westmoreland, W. Shawn, Tramel, Robert W., and Barber, Jennie, “Modeling Propeller Flow-Fields Using CFD”, AIAA Paper 2008-402, Aerospace Sciences Conference and Exhibit, Reno, NV, January 2008.
  • Hall, L.H., Eppard, W.M., Applebaum, M.P., Mitchell, C.R., “Computational Simulation Techniques of Panel Fairing Jettison from a Launch Vehicle System”, JANNAF 959, 2008.
  • Nichols, R.H and Westmoreland, Shawn, “Comparison of Simulation Approaches for Simulating Flow Inside a Weapons Bay”, AIAA-2006-455, Aerospace Sciences Conference and Exhibit, Reno, NV, January 2006.
  • Adams, R.B., Polsgrove, H, Brown, M.R., et.al, “Nuclear Electric Propulsion Evolution Study – From JIMO to Crewed Outer Planet Missions”, American Nuclear Society, 2005.
  • Westmoreland, Shawn, “A Comparison of Flight Test and CFD for JASSM Jettisons from the B-52”, 7th  Symposium on Overset Composite Grid and Solution Technology, Huntington Beach, CA, October 2004.
  • Lee, J., et al, “Studies of Combined Use of CFD and Wind Tunnel Test Approaches to Simulate a Store Separation from F-15E Using Efficient CFD Database Generation”, AIAA-2004-1474, Applied Aerodynamics Conference and Exhibit, Providence, RI, August 2004.
  • Hall, L.H., “Simulation of Missile with Spinning Tail Fin using Chimera Moving Body Methodology”, AIAA 04-1249, 2004.
  • Batte, Jeff and Westmoreland, Shawn, “Use of CFD-Generated Aerodynamic Data for an F-15E/SLV Flying/Handling Qualities Analysis ” , COMSAC Symposium, NASA Langley Research Center, Sept. 2003
  • Landers, M.G., Hall, L.H., Auman, L.M., “Deflectable Noses and Canard Controls For a Fin-Stabilized Projectile at Supersonic and Hypersonic Speeds”, AIAA 03-3805, 2003.
  • Westmoreland, W., “A Comparison of Inviscid and Viscous Approaches for Store Separations”, AIAA-2002-3258, Applied Aerodynamics Conference and Exhibit, St. Louis, MO, June 2002.
  • Eppard, W. M., McGrory, W.D. and Applebaum, M.P., “The Effects of Water-Vapor Condensation and Surface Catalysis on COIL Performance”, AIAA Paper 2002-2132, 33rd AIAA Plasma dynamics and Lasers Conference, June 20-23 2002.
  • Hall, L.H.., “Chimera Moving Body Methodology for Rolling Airframe Missile Simulation with Dithering Canards”, AIAA 02-2801, 2002.
  • Hall, L.H.., “Rolling Airframe Missile Aerodynamic Predictions Using a Chimera Approach for Dithering Canards”, AIAA 02-0405, 2002.
  • Westmoreland, W. and Roberts, E.,“CFD and Flight Test Comparisons for a Lifting Body Store Separation Transient Event”, ITEA Aircraft/Stores Compatibility Conference, San Destin, FL, 2000.
  • Westmoreland, Shawn, and Gebert, Glenn, “Strake Effectiveness for Controlling Out-of-Plane Loading on Missile Configurations”, AIAA-2000-386, Aerospace Sciences Conference and Exhibit, Reno, NV, January 2000.
  • Landers, M.G., Hall, L.H., Auman, L.M., “Aerodynamic Predictions of Pitch and Roll Control for Canard-Controlled Missiles”, AIAA 00-4516, 2000.
  • Eppard, W. M., McGrory, W.D., Godfrey, A.G., Cliff, E.M. and Borggaard, J.T., “Recent Advances in Numerical Techniques for the Design and Analysis of COIL Systems”, AIAA Paper 2000-2576, 31st AIAA Plasmadynamics and Lasers Conference, June 19-22 2000.
  • Hall, L.H., “Navier-Stokes/6-DOF Analysis of the JDAM Store Separation from the F/A-18C Aircraft”, AIAA 99-0121, Jan. 1999.
  • Brown, M. R., et. al., “Unsteady Flow Ballistics of a Pneumatic Launch Tube,”  AIAA-98-3738.  AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Cleveland, OH, July 13-15, 1998
  • Westmoreland, W.S., and Cinnella, Pasquale, “Limitations of a Reduced Model for the Simulation of Hydrogen/Air Combustion”, AIAA Journal, Vol. 36, No. 9, 1998, pp. 1752-1754.
  • Godfrey, A. G., Eppard, W. M. and Cliff, E. M., “Using Sensitivity Equations for Chemically Reacting Flows”, AIAA Paper 98-4805, 7th AIAA/USAF/NASA/ISSMO Symposium on Multidisciplinary Analysis and Optimization”, September 2-4 1998.
  • Hall, L.H., Parthasarathy, V., “Validation of an Automated Chimera/6-DOF Methodology for Multiple Moving Body Problems”, AIAA 98-0753, 1998.
  • Westmoreland, William Shawn, “Numerical Solution of the Euler Equations with Nonequilibrium Chemistry”, Master’s Thesis, Mississippi State University, May 1997.
  • Brown, M. R., et. al., “A Pneumatic Approach to First Stage Acceleration for Highly Reusable Space Transportation Systems,” AIAA-97-3212. AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Seattle, WA, July 6-9, 1997
  • Brown, M. R., “Unsteady Flow Ballistics of a Pneumatic Launch Tube,” M.S. Thesis, Auburn, AL, December, 1997
  • Hall, L.H., Mitchell, C.R., and Parthasarathy, V., “An Unsteady Simulation Technique for Guidance and Control Applications”, AIAA 97-0636, 1997.
  • Hall, L.H., Mitchell, C.R., “An Unsteady Multi-Body Analysis Technique for Missile Staging Events Using Enriched Structured Grids”, First AFOSR Conference on Dynamic Motion CFD, June 1996.
  •  Eppard, W. M., Mawid, M. A., and Sekar, B., “A Numerical Investigation of Catalytic-Wall Effects on Combustion of High-Speed Flows using GASP Version 3”, Joint Propulsion and Joint Subcommittee Meetings, JANNAF, Dec., 1996.
  • Applebaum, M.P., Walters, R.W., McGrory, W.D., “A Three Dimensional Real Gas Navier-Stokes Method for Unstructured Meshes”, AIAA 33rd Aerospace Sciences Meeting, Reno, NV January, 1995.
  • R. Kretzschmar, S. Mallette, R. Deep, L. Hall, “Aerodynamic Characteristics of Wrap Around Fins on a Tube Launched Tactical Missile,” AIAA 95-1897, 1995.
  • R. Kretzschmar, S. Mallette, R. Deep, L. Hall, “Aerodynamic Effects Due to Body Modifications on a Tube Launched Tactical Missile,” AIAA 95-1896, 1995.
  • Applebaum, M.P., “Unstructured Technology for High Speed Flow Simulations”, Ph.D. Dissertation, VPI&SU, December, 1994.
  • Eppard, W. M. and Grossman, B., “A Multi-Dimensional Kinetic-Based Upwind Solver for the Euler Equations”, Paper 93–3303-CP, 11th AIAA Computational Fluid Dynamics Conference, July, 1993.
  • Applebaum, M.P., Mitchell, C.R., Walters, R.W., McGrory. W.D., “Finite-Rate Chemistry for Generalized Discretizations”, AIAA-93-0895 3Ost Aerospace Sciences Meeting. Reno, NV Jan.1993.
  • Applebaum, M.P., Mitchell, C.R., Walters, R.W., McGrory. W.D., “Application of Thermo-Chemical Models on Unstructured Meshes”, AIAA-93-0895 3Ost Aerospace Sciences Meeting. Reno, NV Jan.1993.
  • Eppard, W. M. and Grossman, B., “An Upwind Kinetic Flux-Vector Splitting Method for Flows in Chemical and Thermal Non-Equilibrium”, Paper 93–0894, AIAA 31st Aerospace Sciences Meeting, Jan. 1993.
  • Grossman, B., and Eppard, W. M., “Kinetic Flux-Vector Splitting for Flows in Chemical and Thermal Non-Equilibrium”, Paper CI-6, 1992 Division of Fluid Mechanics Annual Meeting, American Physical Society, Nov. 1992, Bulletin of APS, 37, No. 8, 1992, p. 1736.
  • Grossman, B., Cinnella, P., and Eppard, W. M., “New Developments Pertaining to Algorithms for Non-Equilibrium Hypersonic Flows”, Computational Fluid Dynamics J., No. 2, July 1992, pp. 175–186.
  • Grossman, B., Cinnella, P., and Eppard, W. M., “Algorithms for Non-Equilibrium Hypersonic Flows”, Proceedings of the 4th International Symposium on Computational Fluid Dynamics, pp. 443–448, Davis CA, Sept. 1991.
  • Eppard, W. M., and Grossman, B., “Calculation of Hypersonic Shock Structure Using Flux-Split Algorithms”, ICAM Report 91–07–04, Virginia Polytechnic Institute and State University, Blacksburg VA, July 1991.
  • Grossman, B., Cinnella, P. and Eppard, W. M., “Flux-Split Methods in Non-Equilibrium Flow”, Proceedings of the International Conference on Mathematical Models and Numerical Methods in Continuum Mechanics, ed. V. M. Fomin, Novosibirsk, U.S.S.R., May 1991.

Flight Mechanics and GN&C

  • Hall, R. A., Hough, S., Orphee, C., and Clements, K., “Design and Stability of an On-Orbit Attitude Control System Using Reaction Control Thrusters”, AIAA Guidance, Navigation, and Control Conference, AIAA SciTech Forum, AIAA 2016-0087.
  • Hall, C. et al., “Ares I Flight Control System Overview,” 2008 AIAA Guidance, Navigation, and Control Conference and Exhibit, AIAA 2008-0000.
  • Norris, L., Tao, Y.C., Hall, R.A., Chuang, J., and Whorton, M., “Analysis of Ares 1 Ascent Guidance Navigation Options,” 2008 AIAA Guidance, Navigation, and Control Conference and Exhibit, AIAA 2008-6290.
  • Jang, J.W., Hall, R.A., and Bedrossian, N., “Ares-I Bending Filter Design Using a Constrained Optimization Approach,” 2008 AIAA Guidance, Navigation, and Control Conference and Exhibit, AIAA 2008-6289.
  • Whorton, M., Yang, L., and Hall, R.A., “Similarity Metrics for Closed-Loop Dynamic Systems,” 2008 AIAA Guidance, Navigation, and Control Conference and Exhibit, AIAA 2008-6624.
  • Hall, R.A., Barrington, R., Kirchwey, K., and Alaniz, A., “Shuttle Stability and Control during the Orbiter Repair Maneuver,” 2005 AIAA Guidance, Navigation and Control Conference and Exhibit, AIAA 2005-5852.
  • Hall, R.A. and Lowry, N.C., “Cost Functions for Bang-Off-Bang Control or Axisymmetric Spacecraft,” 2003 American Astronautical Society Guidance, Navigation and Control Conference,  AAS 03-102.
  • Hall, R.A., and Kaznacheyev, Y., “Fuel-optimal rotations of the space station Mir,” 1996 AIAA Guidance, Navigation, and Control Conference, AIAA 96-3789.
  • Kaznacheyev, Y., Chertok, M.B., and Hall, R.A., “Optimal control for a class of nonlinear systems,” 1995 34th IEEE Conference on Decision and Control, New Orleans, LA, USA, 1995, pp. 3802-3804 vol.4.
  • Walker, S.R., and Hall, R.A., “Space Shuttle Rbar Pitch Maneuver for Thermal Protection System Inspection,” 2005 AIAA Guidance, Navigation and Control Conference and Exhibit, AIAA 2005-5983.
  • Orr, J., and Dennehy, N., “Analysis of the X-15 flight 3-65-97 divergent limit cycle oscillation,” AIAA J. Aircraft, July, 2016 (online, http://dx.doi.org/10.2514/1.C033703).
  • Orr, J. and Slegers, N., “High-efficiency thrust vector control allocation,” Journal of Guidance, Control, and Dynamics, Vol. 37, No. 2 (2014), pp. 374-382, doi:10.2514/1.61644, 2014.
  • Orr, J. and Shtessel, Y., “Lunar spacecraft powered descent control using higher-order sliding mode techniques,” Journal of The Franklin Institute, doi:10.1016/j.j.franklin.2011.06.015, 2012.
  • Miller, C., Orr, J., Hanson, C., and Gilligan, E., “Airborne Simulation of Launch Vehicle Dynamics,” AAS Guidance, Navigation, and Control Conference, Breckenridge, CO, 2015, AAS 15-097.
  • Orr, J., Powers, J., and Yang, H.Q., “Lattice Boltzmann Method for Spacecraft Propellant Slosh Simulation,” AAS Guidance, Navigation, and Control Conference, Breckenridge, CO, 2015, AAS 15-091.
  • Orr, J., Statler, I., and Barshi, I., “The X-15 Flight 3-65 Accident: An Aircraft Systems and Flight Control Perspective”, Proceedings of the 7th Conference of the International Association for the Advancement of Space Safety, Friedrichshafen, Germany, 20-22 October 2014.
  • Barshi, I., Orr, J., and Statler, I., “The Human Factors of an Early Space Accident: Flight 3-65 of the X-15.”  Proceedings of the 7th Conference of the International Association for the Advancement of Space Safety, Friedrichshafen, Germany, 20-22 October 2014.
  • Hanson, C., Miller, C., VanZwieten, T., Gilligan, E., Orr, J., and Wall, J., “Launch Vehicle Manual Steering with Adaptive Augmenting Control: In-Flight Evaluations Using a Piloted Aircraft”, 2015 AIAA Guidance, Navigation, and Control Conference, AIAA-2015-1776.
  • Wall, J., VanZwieten, T., Gilligan, E., Miller, C., Hanson, C., and Orr, J., “In-Flight Suppression of a Destabilized F/A-18 Structural Mode Using the Space Launch System Adaptive Augmenting Control System,” 2015 AIAA Guidance, Navigation, and Control Conference, AIAA-2015-1775.
  • Orr, J., Trevino, L., and Dalton, C., “Advanced Optical Sensor Technology: Launch Vehicle and Spacecraft Applications,” AIAA Atmospheric Flight Mechanics Conference, 16-20 June 2014, AIAA 2014-2540.
  • Orr, J., Wall, J., VanZwieten, T., and Hall, C., “Space Launch System Ascent Flight Control Design,” American Astronautical Society Guidance, Navigation, and Control Conference, Breckenridge, Colorado, 2014, AAS 14-038.
  • Wall, J., Orr, J., and VanZwieten, T., “Space Launch System Implementation of Adaptive Augmenting Control,” American Astronautical Society Guidance, Navigation, and Control Conference, Breckenridge, Colorado, 2014, AAS 14-051.
  • VanZwieten, T., Gilligan, E., Wall, J., Orr, J., Miller, C., and Hanson, C., “Adaptive Augmenting Control Flight Characterization Experiment on an F/A-18”, American Astronautical Society Guidance, Navigation, and Control Conference, Breckenridge, Colorado, 2014, AAS 14-052.
  • Orr, J., “Optimal Recursive Digital Filters for Active Bending Stabilization,” American Astronautical Society Guidance, Navigation, and Control Conference, Breckenridge, Colorado, 2013, AAS 13-054.
  • VanZwieten, T., Hanson, C., Wall, J., Miller, C., Gilligan, E., Orr, J., and Dennehy, N., “Flight Testing of the SLS Launch Vehicle AAC Algorithm on an F/A-18,” NESC RP-13-00847, NASA Engineering and Safety Center, September 2014.
  • Orr, J., Barshi, I., Statler, I., and Dennehy, N., “A Comprehensive Analysis of the X-15 Flight 3-65 Accident,” NESC RP-14-00957, NASA Engineering and Safety Center, September 2014.
  • Orr, J., Powers, J., and Yang, H.Q., “Lattice Boltzmann Method for Simulation of Propellant Dynamics in Microgravity,” Technical report ESSSA-FY14-1807, September 2014.
  • Orr, J., and Powers, J., “Lattice Boltzmann Method for Simulation of Propellant Dynamics in Microgravity, Phase II,” Technical report ESSSA-FY15-1718, September 2014.
  • Orr, J., “Elastic Model Transitions Using Quadratic Inequality Constrained Least Squares,” AIAA Modeling and Simulation Technologies Conference, 13-16 August 2012, AIAA 2012-4561.
  • Orr, J. and VanZwieten, T., “Robust, Practical Adaptive Control for Launch Vehicles,” AIAA Guidance, Navigation, and Control Conference, 13-16 August 2012, AIAA 2012-4549.
  • Orr, J., “A Flight Dynamics Model for a Multi-Actuated Flexible Rocket Vehicle,” AIAA Atmospheric Flight Mechanics Conference, 8-11 August 2011, AIAA 2011-6563.
  • Orr, J. and Wall, J., “Linear Approximation to Optimal Control Allocation for Rocket Nozzles with Elliptical Constraints,” AIAA Guidance, Navigation, and Control Conference, 8-11 August 2011, AIAA 2011-6500.
  • Orr, J., “A Coupled Aeroelastic Model for Launch Vehicle Stability Analysis,” AIAA Atmospheric Flight Mechanics Conference, 2-5 August 2010, AIAA 2010-7642.
  • Shtessel, Y., Hall, C., Baev, S., and Orr, J., “Flexible Modes Control Using Sliding Mode Observers: Application to Ares I,” AIAA Guidance, Navigation, and Control Conference, 2-5 August 2010, AIAA 2010-7565.
  • Orr, J. and Hall, C., “Parametric Optimization of Ares I Propellant Slosh Characteristics Using Frequency Response Criteria,” AIAA Guidance, Navigation, and Control Conference, 10-13 August 2009, AIAA 2009-5963.
  • Orr, J., Johnson, M., Wetherbee, J., and McDuffie, J., “State Space Implementation of Linear Perturbation Dynamics Equations for Flexible Launch Vehicles,” AIAA Guidance, Navigation, and Control Conference, 10-13 August 2009, AIAA 2009-5962.
  • Orr, J. and Shtessel, Y., “Robust Lunar Spacecraft Autopilot Design Using High Order Sliding Mode Control,” AIAA Guidance, Navigation, and Control Conference, 10-13 August 2009, AIAA 2009-6182.
  • Orr, J. and Shtessel, Y., “Robust Control of Lunar Spacecraft Powered Descent Using a Second Order Sliding Mode Technique,” AIAA Guidance, Navigation, and Control Conference, 18-21 August 2008, AIAA 2008-6815.
  • Kulikov, I., Smelyanskiy, V., Mackey, R., Luchinsky, D., and Orr, J., “Estimation of Coriolis Force and Torque Acting on Ares I,” Tech Brief NPO-47326, NASA Jet Propulsion Laboratory, 2008.

Experimental and Theoretical Aerodynamics & Vibroacoustics

  • Harrison, J.R., Castel, A., “Validation of the VA-One Periodic Subsystem Module with the Goal to Increase Accuracy of SEA Subsystems in the High Frequency Regime”, 2016 Spacecraft and Launch Vehicle Dynamic Environments Workshop, El Segundo, CA, June 21-23, 2016
  • Pritchettt, V.E., Mayle, M.N., Blevins,J.A., Crosby, W.A., Purinton, D.C, “Aerodynamic Tests of the Space Launch System for Database Development,” AIAA-2014-1256, 52nd AIAA Aerospace Sciences Meeting, National Harbor, MD, Jan 13-17, 2014.
  • Purinton, D.C., Blevins, J.A, Pritchett, V.E., Haynes, D., Carpenter, M., “Aerodynamic Characterization and Simulation of a Solid Rocket Booster During Reentry Flight,” AIAA-2011-14, 49th AIAA Aerospace Sciences Meeting, Orlando, FL, Jan 4-7, 2011.
  • Reid, J. Z., Lynch, K.P., Thurow, B.S., and Wall, David. “Initial Development of Acetone Laser Induced Fluorescence (LIF) for Aero-Optics,” AIAA Paper 2009-4295, 39th AIAA Fluid Dynamics Conference, San Antonio, TX. June 2009
  • Thompson, Robert and Wall, David. “Counter-Current Shear Layer Vortex Generation,” 59th AIAA Southeastern Region II Student Conference, Cape Canaveral, FL. April 2008
  • Keeter, T.M., Purinton, D.C., “Real-Time Flight Vehicle Simulations: Increasing Speed While Preserving Accuracy,” 2002 Interservice/Industry Training, Simulation, and Education Conference.
  • Auman, L.M., Dahlke, C.W., Purinton, D.C., “Aerodynamic Characteristics of Ribbon Stabilized Grenades,” AIAA 2000-0270, 38th AIAA Aerospace Sciences Meeting, Reno, NV, Jan 10-13, 2000.
  • Whitesides, R.H., Dill, R.A, Purinton, D.C., “Application of Two-phase CFD Analysis to the Evaluation of Asbestos-free Insulation in the RSRM,” AIAA-1997-286, 33rd Joint AIAA/ASME/SAE/ASE Propulsion Conference and Exhibit, Seattle, WA, Jul 6-9, 1997.
  • Whitesides, R.H., Dill, R.A, Purinton, D.C., Sambamurthi, J.K., “Design of a Subscale Propellant Slag Evaluation Motor Using Two-Phase Fluid Dynamic Analysis,” AIAA 96-2780, 32nd Joint AIAA/ASME/SAE/ASE Propulsion Conference and Exhibit, Lake Buena Vista, FL, Jul 1-3, 1996.
  • Whitesides, R.H., Purinton, D.C., Hengel, J.E., Skelley, S.E., “Effects of Slag Ejection on Solid Rocket Motor Performance,” AIAA 95-2724, 1995 Solid Rocket Motor Paper of the Year, 31st Joint AIAA/ASME/SAE/ASEE Propulsion Conference and Exhibit, San Diego, CA, Jul 10-12, 1995.