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Research and Technology | NASA Glenn Research Center

Publications

Dr. Louis A. Povinelli

Current as of Feb. 2009

  1. “Combustion Performance Characteristics of a Laboratory Subsonic Ram-Jet," Povinelli, L. A., Journal Royal Aeronautical Society, September 1960, pp. 564 -566.
  2. “A Review of Turbulent Flame Propagation, “Povinelli, L. A., L’Aerotencnica (Rome), Number 5, Volume XL, October 1960, pp. 272 – 286.
  3. “The Ignition Delay Concept for Recessed Flameholders,” Povinelli, L. A., Combustion and Flame, Volume 4, December 1960, pp. 355 – 356.
  4. “The Spectral Theory of Turbulent Flame Propagation,” Povinelli, L. A., and Fuhs, A. E., 8th International Symposium on Combustion, Williams and Wilkins, 1962, 544 – 566.
  5. “Surface Phenomena in Solid Propellant Combustion,” Povinelli, L. A., and Ciepluch, C., 18th Meeting, JANNAF-NASA-ARPA Solid Propellant Group, Volume 11, June 1962, pp. 387 – 400.
  6. “Emission Spectra of High Pressure Hydrogen Oxygen Combustion,” Burrows, M. C. and Povinelli, L. A., NASA TND-1305, July 1962.
  7. “Effect of Oxidizer Particle Size on Additive Agglomeration,” Povinelli, L. A., NASA TMD-1438, November 1962.
  8. “Alumina Size Distribution from High Pressure Composite Solid Propellant Combustion,” Povinelli, L. A. and Rosenstein, R., AIAA Journal, Volume 2, Number 10, October 1964, pp. 1754 – 1760.
  9. “Influence of Turbulence on the Aerothermodynamic Characteristics of Pre-Mixed Flames,” Povinelli, L. A., Recerche di Aerotermodinanuca Presso L’Instituto del Politecnico di Torino, Filippi, F., High Temperatures in Aeronautics, Milan, 1964.
  10. “Spectrographic Measurement of Composite Propellant Flame Zone Structure,” Povinelli, L. A., 1st ICRPG Combustion Conference, CPIA Publication 68, January 1965, pp. 331 – 333.
  11. “Behavior of Large Aluminum Particles in Composite Propellants,” Povinelli, L. A., CPIA Publication 68, January 1965, pp. 373 -376.
  12. “Study of Transverse Mode Solid Propellant Combustion Instability,” Povinelli, L. A., and Heidmann, M., CPIA Publication 68, January 1965, Volume 1, pp. 409 – 411.
  13. “Study of Composite Propellant Flame Zone Structure Using a Spectral-Radiation Shadowgraph Technique,” Povinelli, L. A., AIAA Journal, Volume 3, Number 9, September, 1965, pp. 1593 – 1598.
  14. “Non-Linear Combustion Stability Limits for Solid Propellant Motors Including Vortex Flow Effects,” Povinelli, L. A., CPIA Publication 105, May 1966, pp. 761 – 767.
  15. “One-Dimensional Non-Linear Model for Determining Combustion Instability in Solid Rocket Motors,” Povinelli, L. A., NASA TND-3410, April 1966.
  16. “An Experimental Investigation of Transverse Mode Solid Propellant Combustion Instability in a Vortex Burner,” Povinelli, L. A., Heidmann, M. and Feiler, C. E., NASA TND-3708, November 1966.
  17. “Velocity Sensitivity in Transverse Mode Solid Propellant Combustion Instability,” Povinelli, L. A., 3rd ICRPG Combustion Conference, CPIA Publication 138, October 1966, Volume 1, pp. 255 -258.
  18. “Particulate Damping in Solid Rocket Combustion Instability,” Povinelli, L. A., AIAA Journal, Volume 5, Number 10, 1967, pp. 1791 -1796.
  19. “Aluminum Effect on Hydrogen Oxygen Rocket Instability,” Povinelli, L. A., 4th ICRPG Combustion Conference, CPIA Publication 152, October 1967, pp. 311 – 320.
  20. “Additive Effects in Pressure and Velocity Coupled Solid Rocket Instability,” Povinelli, L. A., 4th ICRPG Combustion Conference, CPIA Publication 152, October 1967, pp. 347 – 352.
  21. “Some Aspects of Steady-State Propellant Combustion as Related to Dynamic Coupling Mechanisms,” Povinelli, L. A., NASA TM X-52419, January 1968.
  22. “Solid Propellant Combustion Instability and the Role of Velocity Coupling,” Povinelli, L. A., NASA TND-5395, 1969.
  23. “Summary Report on the Nature of Ammonium Per chlorate Deflagration,” Povinelli, L. A., Proceedings of the 6th ICRPG Combustion Conference, CPIA Publication 192, Volume 1, December 1969, pp. 371 – 374.
  24. “Vortex Enhancement of Jet Penetration in Supersonic Flow,” Povinelli, L. A., Povinelli, F. P. and Hersch, M., AIAA Paper 69 – 664, Also TM X52582.
  25.  “A Study of Helium Penetration and Spreading in a Mach 2 Airstream Using a Delta Wing Injector,” Povinelli, L. A., Povinelli, F. P. and Hersch, M., NASA TND-5322, July 1969.
  26. “Effect of Angle of Attack and Injection Pressure on Jet Penetration and Spreading from a Delta Wing in Supersonic Flow,” Povinelli, F. P., Povinelli, L. A. and Hersch, M., NASA TM X-1889, 1969.
  27. “Optical Study of Sonic and Supersonic Jet Penetration into a Supersonic Stream,” Hersch, M., Povinelli, L. A. and Povinelli, F. P., Journal of Spacecraft and Rockets, Volume 7, June 1970, pp. 755 – 756.
  28. “A Schlieren Technique for Measuring Jet Penetration into a Supersonic Stream,” Hersch, M., Povinelli, L. A. and Povinelli, F. P., Journal of Spacecraft and Rockets, Volume 7, June 1970, pp. 755 – 756.
  29. “Supersonic Jet Penetration (up to Mach 4) into a Mach 2 Airstream,” Journal of Spacecraft and Rockets, Povinelli, F. P., Povinelli, L. A. and Hersch, M., Volume 7, November 8, August 1970, pp. 988 – 992.
  30. “Effect of Interacting Vortices on Jet Penetration into a Supersonic Stream,” Hersch, M. and Povinelli, L. A., NASA TMX-2314, November 1970.
  31. “Correlation of Secondary Sonic and Supersonic Gaseous Jet Penetration into Supersonic Crossflows,” Povinelli, F. P. and Povinelli, L. A., NASA TND-6370, June 1971.
  32. “Jet Penetration into a Mach 2 Airstream Using Sweptback Injectors at Angle of Attack,” Povinelli, L. A., NASA TMX-2319, July 1971.
  33. “Injection into a Supersonic Stream from the Windward Side of Sweptback Injectors at Angle of Attack,” Povinelli, L. A., Journal of Spacecraft and Rockets, Volume 8, Number 10, October 1971, pp. 1101 – 1103.
  34. “Swirling Base Injection for Supersonic Combustion Ramjets,” Povinelli, L. A. and Ehlers, R. C., AIAA Journal, September 1972, Volume 10, Number 9, pp. 1243 – 1244.
  35. “Report of Hypersonic Aircraft Technology Subpanel,” Joint DOD/NASA Aero Research and Development Study (MARD), Becker, J. V. et al., September 1972.
  36. “Introduction by Guest Editor, papers from AIAA/SAE 7th Propulsion Joint Specialist Conference, Povinelli, L. A., NASA TM X-3015, 1974.
  37. “Drag and Distribution Measurements of Single element Fuel Injectors for Supersonic Combustors,” Povinelli, L. A., NASA TM X-3015, 1974.
  38. “Aerodynamic Drag and Fuel Spreading Measurements in a Simulated Scramjet Combustion Module,” Povinelli, L. A., NASA TND-7674, 1974.
  39. “An Aerodynamic Study of Scramjet Fuel Injectors,” Povinelli, L. A., Fluid Mechanics of Combustion, Fluids Engr. Division, 1974, pp. 115 – 133, Edited by Dussord, J. L., Lohmann, R. P. Uram, E. M.
  40. “An Experimental and Analytical Investigation of Axisymmetric Diffusers,” Povinelli, L. A., AIAA Journal, Volume 14, Number 9, September 1976, pp. 1280 – 1285.
  41. “High Performance Vehicle Technology,” Povinelli, L. A., Aero-Propulsion 1979, NASA Conference Publ. 2092, May 1979.
  42. “An Analytical and Experimental Study of a Short S-Shaped Subsonic Diffuser of a Supersonic Inlet,” Neumann, H. E., Povinelli, L. A. and Coltrin, R. E., AIAA Paper 80-0386, also NASA TM 81406.
  43. “Computations of Three-Dimensional Flow in Turbofan Mixers and Comparison with Experimental Data,” Povinelli, L. A., Anderson, B. H. and Gerstemaier, W. H., AIAA Paper 80-0227, also NASA Tech Memo 81410.
  44. “Influence of Pressure Driven Secondary Flows on the Behavior of Turbofan Forced Mixers,” Anderson, B. H., Povinelli, L. A. and Gerstemaier, W., AIAA Paper 80 – 1198.
  45. “Factors Which Influence the Behavior of Turbofan Forced Mixer Nozzles,” Anderson, B. H. and Povinelli, L. A., NASA Tech Memo 81668, AIAA Paper 81 – 0274.
  46. “Three Dimensional Compressible Viscous Analysis of Mixer Nozzles,” Goyal, Blackmore, Head, V. L. and Povinelli, L. A., AIAA Paper 83 – 11401.
  47. “Hot-Flow Tests of a Series of 10-Percent-Scale Turbofan Forced Mixing Nozzles,” Head, V. L., Povinelli, L. A. and Gerstenmaier, W. H., NASA Tech Paper 2268, January 1984.
  48. “Comparison of Secondary Flows Predicted by a Viscous Code and an Inviscid Code with Experimental Data for a Turning Duct,” Schwab, J. R. and Povinelli, L. A., Computation of Internal Flows: Methods & Applications, ASME Fluids Eng. Div., Pub, FED, Volume 14, 1984, pp. 518 – 525.
  49. “Investigation of Mixing in a Turbofan Exhaust Duct, Part II: Computer Code Application and Verification,” Povinelli, L. A. and Anderson, B. A., AIAA Journal, Volume 22, Number 4, April 1984, pp. 518 – 525.
  50. “Application of Viscous and Inviscid Computation Methods for Rocket Turbopump Systems,” Povinelli, L. A., Haas, J. E, McLallin, K. L., Schwab, J. R. and Chima, R. V., SAE Paper 841522, Soc. Auto Engrs SP-593, pp. 39 – 57, December 1984.
  51. Three Dimensional Flow Phenomena in Fluid Machinery, Editors: Hamed, A., Herring, J. and Povinelli, L. A., ASME Fluids Engr. Division Publ. FED, Volume 32, 1985.
  52. “Application of a Quasi-3D Inviscid Flow and Boundary Layer Analysis to the Hub-Shroud Contouring of a Radial Turbine,” Civinskas, K. C. and Povinelli, L. A., AIAA Paper 84 – 1297, also NASA TM 83669.
  53. “Assessment of Three-Dimensional Inviscid Codes and Loss Calculations for Turbine Aerodynamic Computations,” Povinelli, L. A., Journal of Engr. For Gas Turbines and Power, Volume 107, April 1985, pp. 265 – 276.
  54. “Analytical Modeling of Circuit Aerodynamics in the New NASA Lewis Altitude Wind Tunnel,” Towne, C. E., Povinelli, L. A., Kunik, W. G., Muramoto, K. K., Hughes, C. E. and Levy, R., AIAA Paper 85-03880, January 1985 also NASA Tech Memo 86912.
  55. “Analytical and Physical Modeling Program for the NASA Lewis Research Center’s Altitude Wind Tunnel,” Abbott, J. M., Diedrich, J. H., Groeneweg, J. F., Povinelli, L. A., Reid, L., Reinmann, J. J., Szuch, J. R., AIAA Paper 85-0379, January 1985.
  56. “Computation of Three-Dimensional, Rotational Flow Through Turbomachinery Blade Rows for Improved Aerodynamic Design Studies,” Subramanian, S. V., Bozzola, R. and Povinelli, L. A., ASME Paper 86-GT-26, June 2986.
  57. “Validation of Viscous and Inviscid Computational Methods for Turbomachinery Components,” Povinelli, L. A., ASME Paper 86-GT-42, June 1986, also NASA Tech Memo 87193.
  58. “Viscous Analyses for Flow Through Subsonic and Supersonic Intakes,” Povinelli, L. A. and Towne, C. E., AGARD Conference Proceedings No. 400, pp. 5-1 to 5-20, March 1987, NASA TM 88831.
  59. “Retooling CFD for Hypersonic Aircraft,” Dwoyer, D. L., Kutler, P. and Povinelli, L. A., Aerospace America, Vol. 25, No. 10, pp. 32-35, 41, October 1987.
  60. “CFD Validation Experiments for Internal Flows,” Povinelli, L. A., AGARD Fluid Dynamics Panel Meeting, Lisbon, Portugal, May 2, 1988.
  61. “Least-Squares Finite Element Method for Fluid Dynamics,” Kian, Bo-nan and Povinelli, L. A., NASA TM 102352, ICOMP-89-23, August 1989.
  62. “Advanced Computational Techniques for Hypersonic Propulsion,” Povinelli, L. A., Ninth International Symposium on Air Breathing Engines, Athens, Greece, September 4 – 9, 1989, NASA TM 102005.
  63. “Implicit Solution of Three-Dimensional Internal Turbulent Flows,” Michelassi, V., Liou, M.-S., Povinelli, L. A., and Martelli, F., CFD Symposium on Aeropropulsion, NASA Lewis Research Center, Cleveland, Ohio, April 24-26, 1990.
  64. “Third Annual Report of the Institute for Computational Mechanics in Propulsion,” Feiler, C. E., Povinelli, L. A., NASA TM 101961, ICOMP 89-1, 1989.
  65. “Fourth Annual Report of the Institute for Computational Mechanics in Propulsion,” Feiler, C. E.; and Povinelli, L. A., NASA TM 102640, ICOMP 90-1.
  66. “Computational Modeling and Validation for Hypersonic Inlets,” Povinelli, L. A., AGARD Conference Proceedings 479, Madrid, Spain, 1990; also NASA TM 103111.
  67. “Fifth Annual Report of the Institute for Computational mechanics in Propulsion,” Feiler, C. E.; Povinelli, L. A., NASA TM 103790, ICOMP 91-1.
  68. “CFD Propels NASP Propulsion Progress,” Povinelli, L. A., Dwoyer, D. L., and Green, M., Aerospace America, July 1990.
  69. “CFD for Hypersonic Propulsion,” Povinelli, L. A., Workshop on Hypersonic Flow, INRIA-GAMNI-SMAI Antibes, France, January 1990, NASA TM 103791.
  70. “Least Squares Finite Element Method for Fluid Dynamics,” Computational Methods in Applied Mechanics and Engineering, 81, 1990.
  71. “Navier-Stokes Analysis of Transonic Cascade Flow,” Arnone, A., Liou, M.-S., and Povinelli, L. A., NASA TM 103624, ICOMP 90 -23, October 1990.
  72. “Space and Transatmospheric Propulsion Technology,” Japanese Technology Evaluation Center, Panel Report, August 1990, Loyola College, Maryland, Povinelli, L. A., et. al. (editors).
  73. “Multi-Grid Calculations of Three-Dimensional Viscous Cascade Flow,” Arnone, A., Liou, M. –S. and Povinelli, L. A., NASA TM 105247, ICOMP 91-18, October 1991. (Presented at AIAA 9th Applied Aeronautics Conference, September 1991.).
  74. “Application of Computational Fluid Dynamics in High Speed Propulsion,” Povinelli, L. A., NASA TM 103780-IMACS Conference, Dublin, Ireland, July 1991.
  75. “Optimal Least-Squares Finite Element Method for Elliptic Problems,” Jiang, B. –N. and Povinelli, L. A., NASA TM 105382, ICOMP 91-29, December 1991.
  76. “Relationship Between University, Industry and Government – Expectation and Reality,” Panel Presenter, 1991 ASME International Gas Turbine Expo, Orlando, June 1991.
  77. “Navier-Stokes Solution of Transonic Cascade Flows Using Non-Periodic C-Type Grids,” Povinelli, L. Al, Journal Propulsion and Power, Vol. 8, No. 2, March – April 1992.
  78. “CFD Techniques for Propulsion Applications – A Technical Evaluation,” Povinelli, L. A., AGARD Conference Proceedings 510, 77th Symposium, San Antonio, TX, 1992.
  79. “Workshop on Engineering Turbulence Modeling,” Povinelli, L. A., Liou, W. W., Shabbir, A. and Shih, T. –H. (Editors), 1992, NASA Conference Publication 10088.
  80. “Trends in Aeropropulsion Research and Their Impact on Engineering Education,” Reichert, B., Povinelli, L. A. and Glassman, A., ASEE Conference Proceedings, 1992.
  81. “Eight Annual Report for the Institute for Computational Mechanics in Propulsion,” Feiler, C. E. and Povinelli, L. A., NASA TM 106542, ICOMP 94-01.
  82. “The Structure of Supersonic Jet Flow and Its Radiate Sound,” Mankbadi, R. R., Hayder, M. E. and Povinelli, L. A., AIAA Paper 93-0549, 31st Aerospace Sciences Meeting Reno, NV, January 11 – 14, 1993, also AIAA Journal, Vol. 32. No. 5, pp. 897 – 906.
  83. “CFD and PDF Modeling for Hypersonic Propulsion,” 3rd Workshop on the European Hypersonics Database, Sophia Antipolis, France, January 27 – 29, 1993.
  84. “Large-Scale Computation of Incompressible Viscous Flow by Least-Squares Finite Element Method,” Jiang, B. –N., Lin, T. L. and Povinelli, L. A., NASA TM 105904, March 1993.
  85. “Applications of CFD for Hypersonic Propulsion,” by Povinelli, L. A., Instabilities and Turbulence in Engineering Flows, Asphis, D. E., Gatski, T. B. and Hirsh, R. (Editors), Kluwer Publishers, 1993, pp. 333 – 348.
  86. “Numerical Simulations of Three-Dimensional Laminar Flow Over a Backward Facing Step; Flow Near Side Wall,” Steinthorrson, E., Liou, M. –S., Povinelli, L. A. and Arnone, A., AIAA Joint Propulsion Conference, Monterey, CA, 1993.
  87. “Multigrid Time Accurate Integration of the Navier-Stokes Equations,” Arnone, A., Liou, M. –S. and Povinelli, L. A., AIAA CFD Conference, Orland, FL, 1993.
  88. “Optimal Least Squares Finite Element Method for Elliptic Problems,” Jiang, B. –N. and Povinelli, L. A., Computer Methods in Applied Mechanics and Engineering 102 (1993), pp. 199 – 212, North Holland.
  89. “The NASA Computational Fluid Dynamics (CFD) Program – Building Technology to Solve Future Challenges,” Richardson, P., Dwoyer, D.L., Kutler, P. and Povinelli, L. A., AIAA CFD Conference, Orlando, FL., July 1993.
  90. “Numerical Aspects in Computational Aero acoustics,” Mankbadi, R. R., Goodrich, J. W., Hayder, M. E. and Povinelli, L. A., Second U. S. National Congress on Computational Mechanics, Washington, DC, August 16 – 18, 1993.
  91. “Development of an Explicit Multiblock/Multigrid Flow Solver for Viscous Flows in Complex Geometries,” Steinthorsson, E., Liou, M. S., and Povinelli, L. A., AIAA 93-2380, Joint Conference, June 1993.
  92. “Theoretical Study of the Incompressible Navier-Stokes Equations by the Least-Squares Method,” Jiang, B. N., Loh, C. Y. and Povinelli, L. A., NASA TM 106535, ICOMP-94-04, March, 1994.
  93. “Computation of Jet Flow and Acoustics: An Overview,” ASME Symposium on High Speed Jets, August 13 – 18, 1994, Hilton Head, S.C.
  94. “Direct Computation of Sound Radiation by Jet Flow Using Large Scale Equations,” Mankbadi, R. R., Shih, S. H., Hixon R. and Povinelli, L. A., AIAA 95-0680, 33rd Aerospace Sciences Meeting, January 9 – 12, 1995, Reno, NV.
  95. “Integration of Navier-Stokes Equations in the Prediction of Jet Noise,” Mankbadi, R. R., Hixon, R., Shih, S. H. and Povinelli, L. A., NASA Technical Memo 106929, AIAA Aerospace Sciences Meeting, January 1995.
  96. “On the Use of Linearized Euler Equations in the Prediction of Jet Noise,” Mankbadi, R. R., Hixon, R. Shih, S. H. and Povinelli, L. A., NASA Technical Memo 106929, AIAA Aerospace Sciences Meeting, January 1995.
  97. “Least-Squares Finite Element Solutions For Three-Dimensional Backward-Facing Step Flow,” Jiang, B. N., Lin, T. L., and Povinelli, L.A., Comp Fluid Dynamics, Vol. 4, p. 1-19.
  98. “The Origins of Spurious Solutions in Computational Electromagnetics,” Jiang, Ho-Nan, Wu, Jie, and Povinelli, L. A., Journal of Computational Physics, 125, 104-123 (1966).
  99. “Inlet and Propulsion Integration of Scram Propellant Vehicles,” Povinelli, L. A., Aerothermodynamics and Propulsion Integration for Hypersonic Vehicles,” AGARD Report R-813, 1996.
  100. ”Prediction of Flow and Acoustic Fields of a Supersonic Jet,” Shih, S. H., Hixon, D. R., Mankbadi, R. R. and Povinelli, L.A., AIAA Paper 96-0751, 34th Aerospace Sciences Meeting, January 15-18, 1996.
  101. ”Current Lewis Turbomachinery Research: Continuing Our Legacy of Excellence,” Povinelli, L.A., The Wu Chang Hua Memorial Lectureship, XIII International Soc Airbreathing Engine Symposium, TN, September 1997.
  102. ”Numerical Study of Duct Geometry Effect of Radiation of Engine Internal Noise,” Dong, T.Z., Shih, S. H., Povinelli, L. A., and Mankbadi, R.R., AIAA Paper 97-1604.
  103. ”On the Use of Linearized Euler Equations for Supersonic Jet Noise Prediction,” Mankbadi, R. R., Hixon, R., Shih, S. H., and Povinelli, L. A., AIAA Journal vol. 36, No. 2, 1998, pp. 130-147.
  104. ”A Surface-Integral Formulation for Jet Noise Prediction Based on the Pressure Signal Alone,” Mankbadi, R.R., Shih, S. H., Dixon, D.R., Stuart, J. T., and Povinelli, L. A., Journal of Computational Acoustics, Vol. 6, No. 3 (1998) 307-320.
  105. ”Large Scale Simulations of Nonlinear Effects in Jet Noise,” Mankbadi, R. R., Shih, S. H., Hixon, R., and Povinelli, L. A., Journal of Propulsion and Power, 1999, p. 14.
  106. ”Potential Applications of NASA Aerospace Technology to Ground-Based Power Systems” Povinelli, L. A., Welch, G. E., Bakhle, M. A., and Brown, G. V., Paper IS-156, XIV International Symposium on Airbreathing Engines Florence, IT, Sept. 1999.
  107. ”A Study of Hydrogen Air Combustor Using NCC,” Shih, T. H., Norris, Ianetti, Marke, Smith, Liu and Povinelli, L.A., AIAA-2001-0808, January 2001, Reno, NV.
  108. ”Impact of Dissociation and Sensible Heat Release on Pulse Detonation and Gas Turbine Engine Performance,” Povinelli, L. A., NASA TM-2001-21080, ISABE Paper 2001-1212, July 2001, Bangalore, India.
  109. ‘Role of Air-Breathing Pulse Detonation Engines in High Speed Propulsion,” Povinelli, L.A., Lee, J. H., and Anderberg, M. NASA TM 2001-211163, Sept. 2001, IAF Paper-01-S.5.01, Oct. 2001, Toulouse, France.
  110. ”Application of Generalized Wall Function for Complex Turbulent Flows,” Shih, Tsai-Hsing, Povinelli, Louis A., and Liu, Nan-Suey, Journal of Turbulence, JoT 4 (2003) 015.
  111. ”Airbreathing Pulse Detonation Engine Performance,” Povinelli, Louis A., and Yungster, Shaye, 26th Airbreathing Propulsion Subcommittee Mtg., JANNAF Conf., Destin, FL, April 8-12, Destin, FL.
  112. “A Generalized Law of the Wall for Three Dimensional Turbulent Boundary Layer” Shih, Tsan-Hsing, Povinelli, L. A. and Liu, Nan-Suey, Paper presented at the 70th birthday of John Lumley, Cornell University, Ithica, NY.
  113. “Nonlinear Analysis of Airfoil High-Intensity Gust response Using a High-Order Prefactored Compact Code,” Crivellini, A., Golubev, V., Mankbadi, R., Scott, J., Hixon, R. and Povinelli, L. A., AIAA Paper 2002 – 2535, AIAA Aerocoustics Meeting, June 2002.
  114. "Thermodynamic Cycle and CFD Analyses for Hydrogen Fueled Air-Breathing Pulse Detonation Engines,” Povinelli, Louis A. and Yungster, Shaye, AIAA/ASME/SAE/ASEE Joint Propulsion Conference, July 7 -11, Indianapolis, IN.
  115. “Pulse Detonation Engines for High Speed Flight,” Povinelli, L. A., NASA/Tm 2002-211908, also Paper 17-5169, AIAA/AAAF 11th International Conference on Hypersonics, September 29 – October 4, 2002, Orleans, France.
  116. “Real Gas Effects on the Performance of Hydrocarbon-Fueled Pulse Detonation Engines,” Povinelli, L. A. and Yungster, Shaye, AIAA paper 2003-0712, 41st Aerospace Sciences Meeting, January 6 – 9, 2003, Reno, NV.
  117. “A Quantitative Comparison of Delta Wing Vortices in the Near-Wake for Incompressible and Supersonic Free Streams,” Wang, F. Y., Milanovic, I. N., Zaman, K. B. M. Q. and Povinelli, L. A., Journal of Fluids Engineering, Vol. 127, pp. 1071 – 1084, November 2005.
  118. ”An Assessment of Pulse Detonation Engine performance Estimation Methods Based on Experimental Results,” Perkins, D., Povinelli, L. A., Petters, D., Thomas, S., Fitje, J. and Dyer, R., AIAA-2005-3831, 41st AIAA Joint Propulsion Conference, Tucson, AZ, July 10-13, 2005.
  119. “Performance Comparisons of Pulse Detonation, Ramjets, Turbofan and Combined Cycle Engines,” Povinelli, L. A., ISABE-2005-1293, ISABE Proceedings, 2005.
  120. “Pulse Detonation Engines: Chemical and Fluid Dynamic Effects,” Povinelli, L. A., Proceedings of the 10th International Workshop on Combustion and Propellants, November 2005, Paper 08-1, pp. 1 – 8.
  121. “Research Related to Nozzle Plume Effects on Sonic Boom,” Povinelli, L. A., Fundamental Aeronautics Program, 12 Month Program Review, Washington, D.C., Nov. 6, 2008.  CD available.
  122. “Supersonics Project,” Coen, P., Povinelli, L.A., and Civinskas, K., 12 Month Program Review, Washington, D.C., Nov. 6, 2008. CD available
  123.  “Airport Noise and Supersonic Cruise Efficiency- Closing Comments,” Povinelli, L.A., NRA Review Mtg., Ohio Aerospace Institute, Cleveland, OH, Jan. 20, 2009. PBMA Supersonics (SUP) website
  124. “Lightweight Durable Engines – Closing Comments,” Povinelli, L. A., NRA Review Mtg.”, Ohio Aerospace Institute, Cleveland, OH, Jan. 21, 2009. PBMA SUP
  125.  “High Altitude Emissions, Airport Noise and Supersonic Cruise Efficiency – Closing Comments,”  Povinelli, L.A., Ohio Aerospace Institute, Cleveland, OH, Jan. 22, 2009, PBMA SUP
  126.  “Supersonics Project Overview -Airframe Cruise Efficiency,” Povinelli, L.A.,   NRA Review Meeting, National Institute of Aerospace, Hampton, VA., Feb. 3, 2009. PBMA SUP
  127. “Light Weight Durable Aircraft – Closing Comments,” Povinelli, L.A., NRA Review Meeting, National Institute of Aerospace, Hampton, VA, Feb. 4, 2009. PBMA SUP
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