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  1. Baurle, R. A., Alexopoulos, G. A., and Hassan, H. A., "An Assumed Joint PDF Approach for Supersonic Turbulent Combustion," Journal of Propulsion and Power, Vol. 10, Aug. 1994, pp. 473-485.
  2. Baurle, R. A., Alexopoulos, G. A., and Hassan, H. A., "Analysis of Supersonic Combustors with Swept Ramp Injectors," Journal of Propulsion and Power, Vol. 3, March-April 1997, pp. 327-328.
  3. Baurle, R. A., Alexopoulos, G. A., and Hassan, H. A., "Modeling of Supersonic Turbulent Combustion Using Assumed PDFs," Journal of Propulsion and Power, Vol. 10, Nov. 1994, pp. 777-786.
  4. Baurle, R. A., Hsu, A. T., and Hassan, H. A., "Assumed and Evolution PDFs in Supersonic Turbulent Combustion Calculations," Journal of Propulsion and Power, Vol. 11, Nov. 1995, pp. 1132-1138.
  5. Baurle, R. A., Mathur, T., Hsu, K.-Y., Donbar, J. M., and Gruber, M. R., "Lean Blowout Studies in the Cavity-Based Flameholder of a Scramjet Combustor."
  6. Baurle, R. A., Tam, C.-J., and Dasgupta, S., "Analysis of Unsteady Cavity Flows for Scramjet Applications," AIAA 2000-3617, July 2000.
  7. Baurle, R. A., and Girimaji, S. S., "An Assumed PDF Turbulence-Chemistry Closure with Temperature-Composition Correlations," AIAA Paper 99-0928, Jan. 1999.
  8. Baurle, R. A., and Gruber, M. R., "A Study of Recessed Cavity Flowfields for Supersonic Combustion Applications," AIAA Paper 98-0938, Jan. 1998.
  9. Baurle, R. A., Fuller, R. P., White, J. A., Chen, T. H., Gruber, M. R., and Nejad, A.S., "An Investigation of Advanced Fuel Injection Schemes for Scramjet Combustion," AIAA Paper 98-0937, Jan. 1998.
  10. Baurle, R. A., Mathur, T., Gruber, M. R., and Jackson, K. R., "A Numerical and Experimental Investigation of a Scramjet Combustor for Hypersonic Missile Applications," AIAA Paper 98-3121, July 1998.
  11. Baurle, R. A., and Girimaji, S. S., "Assumed PDF Turbulent-Chemistry Closure With Temperature-Composition Correlations," Combustion and Flame, 134 , pp 131-148, 2003.
  12. Billig, F. S., Baurle, R. A., Tam, C.-J., and Wornom, S. F., "Design and Analysis of Streamline Traced Hypersonic Inlets," AIAA 99-4974, Nov. 1999.
  13. Chang, S.-C., Yu, S.-T., Himansu, A., Wang, X.-Y., Chow, C.-Y., and Loh, C.-Y., "The Method of Space-Time Conservation Element and Solution Element -- A New Paradigm for Numerical Solution of Conservation Laws," Computational Fluid Dynamics Review, edited by M.M. Hafez and K. Oshima, World Scientific, Singapore, 1998.
  14. Chang, S. C., Wang, X. Y., and Chow, C.-Y., "The Space-Time Conservation Element and Solution Element Method -- A New High-Resolution and Genuinely Multidimensional Paradigm for Solving Conservation Laws," Journal of Computational Physics, Vol. 156, No. 1, 1999, pp. 89-136.
  15. Chen, M.-H., Gaffney, R., Wu, P.-K., Chen, T. H., and Nejad, A. S., "Numerical Simulations of Axisymmetric Sonic Helium and Hydrogen Injections into a Mach 2 Airstream," AIAA Paper No. 95-0873, Reno, NV., Jan., 1995.
  16. Chen, T. H. and Hancock, R. D., "Two-Dimensional Shear-Layer Entrainment and Interface-Length Measurements," AIAA Journal, Vol. 33, No. 5, pp. 949-950, 1994.
  17. Chen, T. H., Creese, A., Dasgupta, S., Fuller, R. P., and Wu, P.-K., "Combustion and Mixing Studies in Compressible Flows," WL-TR-96-2129, Wright-Patterson AFB, Dayton, Ohio, 1996.
  18. Chen, T. H., Nejad, A. S., Carter, C., and Goss, L. P., "A Technique for Simultaneous Velocity Measurement of Liquid and Gas Phases," AIAA Paper 94-0494, 1994.
  19. Chen, T. H., Roe, L. A., and Nejad, A. S., "A Multi-Function Droplet-Imaging and Velocimetry System for Spray Jets," Journal of Propulsion and Power, Vol. 10, No. 6, Nov-Dec 1994.
  20. Chen, T. H., Smith, C. R., Schommer, D. G., and Nejad, A. S., "Multi-Zone Behavior of Transverse Liquid Jet in High Speed Flow," AIAA 93-0453, January 1993.
  21. Cox, S. K., Fuller, R. P., Schetz, J. A., and Walters, R. W., "Vortical Interactions Generated by an Injector Array to Enhance Mixing in a Supersonic Flow," AIAA Paper 94-0708, 1994.
  22. Cox-Stouffer, S. K., and Gruber, M. R., "Further Investigation of the Effects of 'Aerodynamic Ramp' Design Upon Mixing Characteristics," AIAA 99-2238, June 1999.
  23. Cox-Stouffer, S. K., and Hagenmaier, M. A., "The Effect of Aspect Ratio on Isolator Performance," AIAA 2001-0519, Jan. 2001.
  24. Cox-Stouffer, S. K., and Mathur, T., "An Innovative Fuel Injection System for Improved Mixing and Penetration in Scramjet Combustors," AFRL-PR-WP-TR-2000-2058.
  25. Cox-Stouffer, S. K., Gruber, M. R., and Bulman, M. J., "A Streamlined, Pressure-Matched Fuel Injector for Scramjet Application," AIAA 2000-3707, July 2000.
  26. Cox-Stouffer, S. K., and Gruber, M. R., "Effects of Injector Yaw on Mixing Characteristics of Aerodynamic Ramp Injectors," AIAA Paper 99-0086, Jan. 1999.
  27. Cox-Stouffer, S. K., and Gruber, M. R., "Effects of Spanwise Injector Spacing on Mixing Characteristics of Aerodynamic Ramp Injectors," AIAA Paper 98-3272, July 1998.
  28. Cox-Stouffer, S. K., and Gruber, M. R., "Further Investigation of the Effects of 'Aerodynamic Ramp' Design Upon Mixing Characteristics," AIAA Paper 99-2238, June 1999.
  29. Dasgupta, S., Chen, T. H., Carter, C., and A. S. Nejad, A. S., "Non-Intrusive Emission Measurements for Combustion Control" AIAA Paper 95-2651, July 1995.
  30. Dasgupta, S., Terry, W. F., Vuppuladhadium, R., Chen, T. H., Bowersox, R. D. W., Glawe, D. D., and Nejad, A. S., "A Two-color Particle Imaging Velocimetry System for Supersonic Flow Studies," AIAA Paper 96-2798.
  31. Dasgupta, S., Wu, P.K., Carter, C., and Nejad, A. S., "Raman Scattering Study of Ethylene Near Super-critical Conditions," AIAA Paper 95-2551, July 1995.
  32. Dasgupta, S., Zhou, J., Boyd, J. T., Jackson, H., Glawe, D. D., and Rivir, R. B., "Optically Integrated Micromachined Sensor Arrays for Propulsion Applications," Proceedings of the 45th International Instrumentation Symposium, Instrumentation Society of America, Research Triangle Park, NC, 1999, 503-510.
  33. Dasgupta, S., Zhou, J., Boyd, J. T., Jackson, H., Glawe, D. D., and Rivir, R. B., "Optically Integrated MEMS Pressure Sensors for Propulsion Applications," submitted to Applied Optics .
  34. Eklund, D. R., Baurle, R. A., and Gruber, M. R., "Numerical Study of a Scramjet Combustor Fueled by and Aerodynamic Ramp Injector in Dual-Mode Combustion," AIAA 2001-0379, Jan. 2001.
  35. Eklund, D. R., Baurle, R. A., and Jackson, T. A., "Investigation of Wall Temperature Effects in a Supersonic Combustor," APS-CS-2H-06.
  36. Eklund, D. R, and Gruber, M. R., "Study of a Supersonic Combustor Employing an Aerodynamic Ramp Pilot Injector," AIAA Paper 99-2249, June 1999.
  37. Eklund, D. R., Badinand, T., and Fransson, T., "A Numerical Study of Radiation Effects in Gas Turbine Combustion Chambers," AIAA Paper 98-3822, July 1998.
  38. Elliott, G., Gruber, M., Nejad, A., and Carter, C., "The Study of a Transverse Jet in a Supersonic Cross-Flow Using Molecular Filter Based Diagnostics," AIAA Paper 97-2999, July 1997.
  39. Fuller, R. P., "Fuel-Vortex Interactions for Enhanced Mixing in Supersonic Flow," Ph.D. Dissertation, Virginia Polytechnic Institute and State University, 1996.
  40. Fuller, R. P., Wu, P.-K., Kirkendall, K. A., and Nejad, A. S., "Effects of Injection Angle on the Breakup Processes of Liquid Jets in Subsonic Crossflows," AIAA Paper 97-2966, Seattle, WA., Jul., 1997.
  41. Fuller, R. P., Wu, P.-K., Nejad, A. S., and Schetz, J. A., "Fuel-Vortex Interactions for Enhanced Mixing in Supersonic Flow," AIAA 96-2661, Orlando, FL., July, 1996.
  42. Glawe, D. D., Goss, L. P., Gogineni, S. P., Bowersox, R. D. W., Terry, W. F. and Dasgupta, S. "Digital Two-Color PIV Measurements in a Mach-2.8 Boundary Layer," AIAA Paper 96-2799, 1996.
  43. Glawe, D. D., Samimy, M., Nejad, A. S., and Chen, T. H. "Effects Of Nozzle Geometry On Parallel Injection From Base Of An Extended Strut Into Supersonic Flow," AIAA Paper 95-0522, 1995.
  44. Gruber, M. R. and Nejad, A. S., "Development of a Large-Scale Supersonic Combustion Research Facility," AIAA Paper 94-0544, January 1994.
  45. Gruber, M. R., and Nejad, A. S., "New Supersonic Combustion Research Facility," Journal of Propulsion and Power, Vol. 11, No. 5, 1995, pp. 1080-1083.
  46. Gruber, M. R., Baurle, R. A., Mathur, T., and Hsu, K.-Y., "Fundamental Studies of Cavity-Based Flameholder Concepts for Supersonic Combustors," Journal of Propulsion and Power, Vol. 17, No. 1, pp. 146-153.
  47. Gruber, M. R., Nejad, A. S., and Dutton, J. C., "Circular and Elliptical Transverse Injection into a Supersonic Crossflow--The Role of Large-Scale Structures," AIAA Paper 95-2150, June 1995.
  48. Gruber, M. R., Nejad, A. S., and Goss, L. P., "Surface Pressure Measurements in Supersonic Transverse Injection Flowfields," AIAA Paper 97-3254, July 1997.
  49. Gruber, M. R., Nejad, A. S., Chen, T. H., and Dutton, J. C., "Bow Shock-Jet Interaction in Compressible Transverse Injection Flowfields." AIAA Journal, Vol. 34, No. 10, 1996, pp. 2191-2193.
  50. Gruber, M. R., Nejad, A. S., Chen, T. H., and Dutton, J. C., "Compressibility Effects in Supersonic Transverse Injection Flowfields," Physics of Fluids, Vol. 9, No. 5, 1997, pp. 1448-1461.
  51. Gruber, M. R., Nejad, A. S., Chen, T. H., and Dutton, J. C., "Large Structure Convection Velocity Measurements in Compressible Transverse Injection Flowfields," AIAA Paper 96-0203, January 1996.
  52. Gruber, M. R., Nejad, A. S., Chen, T. H., and Dutton, J. C., "Large Structure Convection Velocity Measurements in Compressible Transverse Injection Flowfields," Experiments in Fluids, Vol. 22, 1997, pp. 397-407.
  53. Gruber, M. R., Nejad, A. S., Chen, T. H., and Dutton, J. C., "Mixing and Penetration Studies of Sonic Jets in a Mach 2 Freestream," AIAA Paper 94-0709, January 1994.
  54. Gruber, M. R., Nejad, A. S., Chen, T. H., and Dutton, J. C., "Mixing and Penetration Studies of Sonic Jets in a Mach 2 Freestream, " Journal of Propulsion and Power, Vol. 11, No. 2, 1995, pp. 315-323.
  55. Gruber, M., Donbar, J., Donaldson, W., Jackson, T., Mathur, T., Eklund, D., and Billig, F., "Performance of an Aerodynamic Ramp Fuel Injector in a Scramjet Combustor," JANNAF, Oct. 1999
  56. Gruber, M., Donbar, J., Jackson, T., Mathur, T., Eklund, D., and Billig, F., "Performance of an Aerodynamic Ramp Fuel Injector in a Scramjet Combustor," AIAA 2000-3708, July 2000.
  57. Gruber, M., Jackson, K., Mathur, T., and Billig, F., "Experiments with a Cavity-Based Fuel Injector for Scramjet Applications," Paper IS-7154, International Symposium on Air-Breathing Engines, Sept. 1999.
  58. Gruber, M. R., Baurle, R. A., Mathur, T., and Hsu, K.-Y., "Fundamental Studies of Cavity-Based Flameholder Concepts for Supersonic Combustors," AIAA Paper 99-2248, June 1999.
  59. Himansu, A., Chang, S.-C., Yu, S.-T., Wang, X.-Y., Loh, C.-Y., and Jorgenson, P. C. E., "High-Resolution and Genuinely Multidimensional Solution of Conservation Laws by the Space-Time Conservation Element and Solution Element Method," AIAA Paper 99-1006, Jan. 1999.
  60. Himansu, A., Jorgenson, P. C. E., Wang, X. Y., and Chang, S. C., "Parallel CE/SE Computations via Domain Decomposition," NASA/TM-2000-210480.
  61. Himansu, A., Freeh, J. E., Steffen, C. J., Jr., Tornabene, R. T., and Wang, X, -Y., "Hybrid Solid Oxide Fuel Cell / Gas Turbine System Design For High Altitude Long Endurance Aerospace Missions," Proceedings of FUELCELL2006, 4th International ASME Conference on Fuel Cell Science, Engineering and Technology, June 19-21, 2006, Irvine, California.
  62. Hsu, K.-Y., Carter, C., Crafton, J., Gruber, M., Donbar, J., Mathur, T., Schommer, D., and Terry, W., "Fuel Distribution About a Cavity Flameholder in Supersonic Flow," AIAA 2000-3585.
  63. Jackson, K., Gruber, M., Mathur, T., Streby, G., Smith, C., and Billig, F., "Calibration of a Newly Developed Direct-Connect High-Enthalpy Supersonic Combustion Research Facility," AIAA Paper 98-1510, April, 1998.
  64. Lin, K.-C., Kennedy, P. J., and Jackson, T. A., "Spray Penetration Heights of Angled-Injected Aerated-Liquid Jets in Supersonic Crossflows," AIAA 2000-0194, Jan. 2000.
  65. Lin, K.-C., Kennedy, P. J., and Jackson, T. A., "Spray Structures of Aerated Liquid Jets in Supersonic Crossflows," AIAA 2001-0330, Jan. 2001.
  66. Lin, K.-C., Kennedy, P. J., and Jackson, T. A., "Structures of Aerated Liquid Fuel Jets Interacting with a Shock Train in Supersonic Crossflows," Eighth International Conference on Liquid Atomization and Spray Systems, July 2000.
  67. Lin, K.-C., Kirkendall, K. A., Kennedy, P. J., and Jackson, T. A., "Spray Structures of Aerated Liquid Fuel Jets in Supersonic Crossflows," AIAA Paper 99-2374, June 1999.
  68. Lin, K.-C., Kennedy, P. J., and Jackson, T. A., "Spray Penetration Heights of Angled-Injected Aerated Liquid Fuel Jets in Supersonic Crossflows," AIAA Paper 2000-0194, 38th Aerospace Sciences Meeting & Exhibit, Jan 2000.
  69. Edwards, J. R., Pinto, A. M., Lin, K.-C., and Jackson, T. A., "Simulation of Injection of Supercritical Methane / Ethlene Mixtures into Nitrogen," AIAA Paper 2003-4267, 33rd AIAA Fluid Dynamics Conferences and Exhibit, June 2003.
  70. Lin, K.-C., Kennedy, P. J., and Jackson, T. A., "Structures of Water Jets in a Mach 1.94 Supersonic Crossflow," AIAA Paper 2004-0971, 42nd AIAA Aerospace Sciences Meeting and Exhibit, Jan 2004.
  71. Liou, M.-S., and Zheng, Y. , "Development of 3D DRAGON Grid Method for Complex Geometry," Frontiers of Computational Fluid Dynamics - 2000, edited by D. A. Caughey and M. M. Hafez, World Scientific Publishing Company PTE. Ltd., Singapore, 2000, pp. 1-19.
  72. Liou, M.-S., and Zheng, Y., "A Three-Dimensional Hybrid Grid: DRAGON Grid,"
  73. Loh, C. Y., Himansu, A. , Wang, X. Y., Jorgenson, P. C. E., "Computation of an Underexpanded 3-D Rectangular Jet by the CE/SE Method," AIAA 2001-0986, Jan. 2001.
  74. Loh, C.-Y., "Computational Aeroacoustics by the Space-Time CE/SE Method," NASA/CR-2001-210680.
  75. Loh, C.-Y., and Hui, W. H., "A New Lagrangian Method for Time-Dependent Inviscid Flow Computations," J. Sci. Comput., Vol. 22, No. 1, pp. 330-350.
  76. Loh, C.-Y., Chang, S.-C., Wang, X.-Y, and Jorgenson, P. C. E., "GAP Noise Computation by the CE/SE Method," NASA/TM-2001-210703, FEDSM-2001-18136.
  77. Loh, C.-Y., Himansu, A., Wang, X.-Y, and Jorgenson, P. C. E., "Computation of an Underexpanded 3-D Rectangular Jet by the CE/SE Method," AIAA 2001-0986, Jan. 2001.
  78. Loh, C.-Y., Hultgren, L. S., and Jorgenson, P. C. E., "Near Field Screech Noise Computation for an Underexpanded Supersonic Jet by the CE/SE Method," AIAA 2001-2252.
  79. Loh, C.-Y., Wang, X.-Y, Chang, S.-C., and Jorgenson, P. C. E., "Computation of Feedback Aeroacoustic System by the CE/SE Method," NASA/TM-2000-210479.
  80. Loh, C. Y., Hultgren, L.S., and Chang, S.-C., "Computing Waves in Compressible Flow Using the Space-Time Conservation Element and Solution Element Method," AIAA Paper 98-0369, Jan. 1998.
  81. Loh, C. Y., Hultgren, L.S., and Chang, S.-C., "Wave Computation in Compressible Flow Using the Space-Time Conservation Element and Solution Element Method," AIAA Journal, submitted.
  82. Loh, C. Y., Hultgren, L.S., Chang, S.-C., and Jorgenson, P. C. E., "Noise Computation for a Shock-Containing Supersonic Axisymmetric Jet Using the CE/SE Method," AIAA Paper 2000-0475, Jan. 2000.
  83. Loh, C. Y., Hultgren, L.S., Chang, S.-C., and Jorgenson, P. C. E., "Vortex Dynamics Simulation in Aeroacoustics by the Space-Time Conservation Element and Solution Element Method," AIAA 99-0359, Jan. 1999.
  84. Loh, C. Y., Hultgren, L. S., Wang, X. Y., Chang, S.-C., and Jorgenson, P. C. E., "Aeroacoustics Computation for Nearly Fully Expanded Supersonic Jets Using the CE/SE Method," AIAA Paper 2000-2010, June 2000.
  85. Loh, C. Y., Wang, X. Y., Jiang, B. N., Chang, S.-C., and Jorgenson, P. C. E., "Generation and Radiation of Acoustic Waves from a 2-D Shear Layer Using the CE/SE Method," 3rd Computational Aeroacoustics Workshop, Nov. 1999. Proceedings to appear.
  86. Loh, C. Y., Chang, S.-C., Wang, X. Y., and Jorgenson, P. C. E., "GAP Noise Computation by the CE/SE Method," NASA/TM-2001-210703, Feb 2001
  87. Loh, C. Y., Hultgren, L. S., and Jorgenson, P. C. E., "Near Field Screech Noise Computation for An Underexpanded Supersonic Jet by the CE/SE Method," AIAA Paper 2001-2252, 7th AIAA/CEAS Aeroacoustics Conference, May 2001.
  88. Loh, C. Y., and Zaman, K.B.M.Q., "Numerical Investigation of 'Transonic Resonance' with A Convergent-Divergent Nozzle," AIAA Paper 2002-0077, 40th AIAA Aerospace Sciences Meeting & Exhibit, Jan 2002.
  89. Loh, C. Y. "On a Non-Reflecting Boundary Condition for Hyperbolic Conservation Laws," AIAA Paper 2003-3975, 16th AIAA Computational Fluid Dynamics Conference and the 33rd Fluid Dynamics Conference and Exhibit, Jun 2003.
  90. Loh, C. Y., “Computation of Low Speed Cavity Noise,” AIAA 2004-0680, 42nd AIAA Aerospace Sciences Meeting and Exhibit, Jan 2004.
  91. Mathur, T., Cox-Stouffer, S., Hsu, K.-Y., Crafton, J., Donbar, J., and Gruber, M., "Experimental Assessment of a Fuel Injector for Scramjet Applications," AIAA 2000-3703, July 2000.
  92. Mathur, T., Lin, K.-C., Kennedy, P., Gruber, M., Donbar, J., Jackson, T., and Billig, F., "Liquid JP-7 Combustion in a Scramjet Combustor," AIAA 2000-3581, July 2000.
  93. Mathur, T., Streby, G., Gruber, M., Jackson, K., Donbar, J., Donaldson, W., Jackson, T., Smith, C., and Billig, F., "Supersonic Combustion Experiments with a Cavity-Based Fuel Injector," AIAA Paper 99-2102, June, 1999.
  94. Schetz, J. A., Cox-Stouffer, S., and Fuller, R., "Integrated CFD and Experimental Studies of Complex Injectors in Supersonic Flows," AIAA Paper 98-2780, June 1998.
  95. Tam, C.-J., and Baurle, R. A., "Inviscid CFD Analysis of Streamline Traced Hypersonic Inlets at Off-Design Conditions," AIAA 2001-0675, Jan. 2001.
  96. Tam, C.-J., and Hagenmaier, M. A., "Unsteady Analysis of Scramjet Inlet Flowfields using Numerical Simulations," AIAA Paper 99-0613, Jan. 1999.
  97. Tam, C.-J., Baurle, R. A., and Gruber, M. R., "A Numerical Study of Jet Injection into a Supersonic Crossflow," AIAA Paper 99-2254, June 1999.
  98. Wang, X. Y., Himansu, A., Jorgenson, P., and Chang, S. C., "Gust Acoustic Response of a Swept Rectilinear Cascade Using the Space-Time CE/SE Method," FEDSM 2001-18134, May 2001.
  99. Wang, X. Y., and Chang, S. C., "A 2D Non-Splitting Unstructured Triangular Mesh Euler Solver Based on the Space-Time Conservation Element and Solution Element Method," Computational Fluid Dynamics Journal, Vol. 8, No. 2, 1999, pp. 309-325.
  100. Wang, X. Y., Chow, C.-Y., and Chang, S. C., "The Space-Time Conservation Element and Solution Element Method -- A New High-Resolution and Genuinely Multidimensional Paradigm for Solving Conservation Laws, Vol. I The Two Dimensional Time Marching Schemes," NASA TM-1998-208843, Dec. 1998.
  101. Wang, X. Y., Chow, C.-Y., and Chang, S. C., "The Space-Time Conservation Element and Solution Element Method -- A New High-Resolution and Genuinely Multidimensional Paradigm for Solving Conservation Laws, Vol. II Numerical Simulation of Shock Waves and Contact Discontinuities," NASA TM-1998-208843, Dec. 1998.
  102. Wu, P.-K., Chen, M.-H., Baurle, R. A., Eakins, W.E., Chen, T. H., and Nejad, A. S., "Effects of Incorporating a Cone Swirler into a Side-Inlet Ducted Ramrocket," Journal of Propulsion and Power, Vol. 13, No. 1, pp. 162-164, 1997.
  103. Wu, P.-K., Chen, M.-H., Chen, T. H., Nejad, A. S., "Flowfield in Side-Inlet Ducted Rockets with and without Swirler," AIAA Paper 95-2478, July 1995.
  104. Wu, P.-K., Chen, T. H., Nejad, A. S., and Carter C., "Injection of Supercritical Ethylene in Nitrogen," AIAA Paper No. 95-0382, Jan. 1995.
  105. Wu, P.-K., Chen, T. H., Nejad, A. S., and Carter, C.D., "Injection of Supercritical Ethylene in Nitrogen," Journal of Propulsion and Power, Vol. 12, No. 4, 1996, pp. 770-777.
  106. Wu, P.-K., Kirkendall, K. A., Fuller, R. P., and Nejad, A. S., "Breakup Processes of Liquid Jets in Subsonic Crossflows," AIAA Paper 96-3024, July 1996.
  107. Wu, P.-K., Kirkendall, K. A., Fuller, R. P., and Nejad, A. S., "Breakup Processes of Liquid Jets in Subsonic Crossflows," Journal of Propulsion and Power, Vol. 13, No. 1, pp. 64-73, 1996.
  108. Wu, P.-K., Kirkendall, K. A., Fuller, R. P., and Nejad, A. S., "Breakup Processes of Liquid Jets in Subsonic Crossflows," Journal of Propulsion and Power, Vol. 13, No. 1, pp. 64-73, 1997.
  109. Wu, P.-K., Kirkendall, K. A., Fuller, R. P., Gruber, M. R., and Nejad, A. S., "Spray Trajectories of Liquid Fuel Jets in Subsonic Crossflows," 7th International Conference on Liquid Atomization and Spray Systems, Seoul, Korea, Aug., 1997.
  110. Wu, P.-K., Shahnam, M., Kirkendall, K. A., Carter, C.D., and Nejad, A. S., "Expansion and Mixing Processes of Underexpanded Supercritical Fuel Jets Injected into Superheated Conditions," AIAA Paper 97-2852, July 1997.
  111. Wu, P.K., Kirkendall, K. A., Fuller, R. P., Gruber, M. R., and Nejad, A. S., "Spray Trajectories of Liquid Jets in Subsonic Crossflows," Submitted to ICLASS-97 Conference, 1997.
  112. Zheng, Y., and Liou, M.-S., "Progress in the Three-Dimensional DRAGON Grid Scheme," AIAA 2001-2540, June 2001.
  113. Zheng, Y., and Liou, M.-S., "Three-Dimensional DRAGON Grid Methodology: An Approach of Hybrid Grid Schemes," Proceedings of the Fourth Asian Computational Fluid Dynamics Conference, edited by H. Zhang, Univ. of Electronic Science and Technology of China Press, Chengdu, Sichuan, China, 2000, pp. 523-529.
  114. Zheng, Y., Liou, M.-S., and Civinskas, K. C., "Development of Three-Dimensional DRAGON Grid Technology," NASA/TM-1999-209458.
  115. Zheng, Y., Liou, M.-S., and Civinskas, K. C., "Development of Three-Dimensional DRAGON Grid Technology," NASA TM-1999-209458, Oct. 1999.
  116. " Anish Saran, Don C. Abeysinghe, and Joseph T. Boyd, "Anodic Bonding of Optical Fibers-to-Silicon for Integrating MEMS Devices and Optical Fibers", accepted for presentation and publication at IEEE Transducers 03, The 12th International Conference on Solid State Sensors, Actuators and Microsystems, Boston, Massachusetts, June 08-12, 2003. "
  117. Weizhuo Li, Don C. Abeysinghe, J. T. Boyd, "Wavelength Multiplexing of MEMS Pressure and Temperature Sensors Using Fiber Bragg Gratings and Arrayed Waveguide Gratings", Journal of Optical Engineering, Vol. 42, No.2,2003. "
  118. Anish Saran, Don C. Abeysinghe, and Joseph T. Boyd, "Anodic Bonding of Optical Fibers-to-Silicon for Integrating MEMS Devices and Optical Fibers", published in the Journal of Microelectronics and Micromechanics, Vol. 13, No. 02, pp 346-351, 2003. "
  119. Weizhuo Li, Don C. Abeysinghe, J. T. Boyd, "Simultaneous Measurement of Pressure and Temperature with MEMS Sensors", submitted for publication in the Journal of Optical Engineering. "
  120. Don C. Abeysinghe, David Klotzkin, "Adhesive-free method for Fiber Pig-tailing of Optoelectronic Devices and for Silicon Optical Bench Applications", in preparation for submission to Photonic Technology Letters. "
  121. Don C. Abeysinghe, S. Dasgupta, J. T. Boyd, and H. E. Jackson, "Novel MEMS Pressure and Temperature Sensors Fabricated on optical Fibers", Journal of Microelectronics and Micromechanics, pp. 993-995, Vol. 12, No 03, May 2002. "
  122. Don C. Abeysinghe, S. Dasgupta, J. T. Boyd, and H. E. Jackson, " A Novel MEMS Pressure Sensor Fabricated on an optical Fiber", IEEE Photonic Technology Letters, Vol. 13, No. 09, September 2001.
  123. Loh, Ching Y., and Jorgenson, C. E., "A Ronbust Absorbing Boundary Condition for Copressible-Flows," AIAA 2005-4716, AIAA CFD Conference, 2005.
  124. Loh, Ching Y., and Hultgren, Lennart S., "Near-Field Noise Computation for A Supersonic Circular Jet," AIAA 2005-3042.
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