Analytical Services & Materials, Inc.

List of Publications


  1. Abdol-Hamid, K. S.: Development of Three-Dimensional Code for the Analysis of Jet Mixing Problem. NASA CR 4200, December 1988.
  2. Abdol-Hamid, K.S.: Three-Dimensional Calculations for Underexpanded and Over expanded Supersonic Jet Flows, AIAA Paper 89-2196, September 1989.
  3. Abdol-Hamid, K. S.: The Application of 3D Marching Scheme for the Prediction of Supersonic Free Jets. AIAA/ASME/SAE/ASEE 25th Joint Propulsion Conference, Monterey, CA July1989.
  4. Abdol-Hamid, K. S. and Compton, W. B, III: Supersonic Navier-Stokes Simulations of Turbulent Afterbody Flows. AIAA 7th Applied Aerodynamics Conference, AIAA 89-2194, Seattle, Washington August 1989.
  5. Abdol-Hamid, K.S.: A Multiblock/Multizone code (PAB3D-v2) for the Three-Dimensional Navier-Stokes Equations: Preliminary Applications, NASA CR-182032, 1990.
  6. Lakshmann, B. and Tiwari, S. N.: Application of an Improved Two-Equation Turbulence Model for Compressible Mixing Layer/Jet Plumes. Progress Report under Research Contract NAS1-18584-106 Old Domenion University November 1990.
  7. Pao, S. P.; and Abdol-Hamid, Khaled S.: Application of a New Adaptive Grid for Aerodynamic Analysis of Shock Containing Single Jets. AIAA Paper 90-2025, AIAA/SAE/ASME/ASEE 26th Joint Propulsion Conference, Orlando, FL, July 1990.
  8. Compton, W.B.,III and Abdol-Hamid, K.S.: Navier-Stokes Simulations of Transonic Afterbody Flows with Jet Exhaust, AIAA Paper 90-3057, August 1990.
  9. Abdol-Hamid, K.S.:Applictaion of a Multiblock/Multizone Code (PAB3D) for The Three-Dimensional Navier-Stokes Equations. 27th Joint Propulsion Conference AIAA 91-2155, Sacramento, California June 1991.
  10. Uenishi, K. and Abdol-Hamid, K.: A Three-Dimensional Upwinding Navier-Stokes Code with k-e Model for Supersonic Flows", AIAA 22nd Fluid and Plasmadynamic Conference, AIAA 91-1669, June 1991.
  11. Compton, W. B, III and Abdol-Hamid, K. S.: Navier-Stokes Simulation of Nozzle -Afterbody Flows With Jets at Off Design Conditions. AIAA 91-3207, September 1991.
  12. Pao, S. P.; and Abdol-Hamid, K. S.: Grid Adaptation to Multiple Functions for Applied Aerodynamic Analysis, Proceedings of the Third International Conference on Numerical Grid Generation, Barcelona, Spain, June 1991.
  13. Abdol-Hamid, Khaled S.; Carlson, John R.; Pao, S. Paul: Computational Analysis of Vented Supersonic Exhaust Nozzles Using a Multiblock/Multizone Strategy. AIAA Paper No. 91-0125. 29th Aerospace Sciences Meeting, January 7-10, 1991.
  14. Carlson, John R.; and Abdol-Hamid, Khaled S.: Prediction of Internal Performance for Two-Dimensional Convergent-Divergent Nozzles. AIAA Paper No. 91-2369, AIAA/SAE/ASME/ASEE 27th Joint Propulsion Conference, June 24-27, 1991.
  15. Pao, S. Paul; Abdol-Hamid, Khaled S.; and Carlson, John R.: Computational Investigation of Circular-To-Rectangular Transition Ducts. AIAA Paper No. 91-3342, AIAA 9th Applied Aerodynamics Conference September 23-25, 1991.
  16. Jones, W. T. and Walkley, K. B.: Numerical Investigation for Drag Reduction on a Single Engine Body-Empennge Model, DEI Report D-396, 1992.
  17. Abdol-Hamid, Khaled S.; Uenishi, K.; Carlson, John R.; Keith, B. D.: Commercial Turbofan Engine Exhaust Nozzle Flow Analysis Using PAB3D. AIAA Paper 92-2701. AIAA 10th Applied Aerodynamics Conference, June 22-24, 1992.
  18. Compton, W. B., III; Abdol-Hamid, K. S. and Abeyounis, W. K.: Comparison of Algebraic Turbulence Models for Flows with Jet Exhaust. AIAA Journal, Vol. 30 No. 11, November 1992.
  19. Carlson, John R.: A Nozzle Internal Performance Prediction Method. NASA TP-3221,1992.
  20. Lakshmann, B. and Abdol-Hamid, K. S.: Application of Space Marching Procedure for Transport Equation of Turbulence Models. Computational Fluid Dynamics Journal, Vo. 1. No.3, October 1992.
  21. Lakshmann, B. and Abdol-Hamid, K. S.: Comparative Study of Two Codes With an Improved Two-Equation Turbulence Model for Predicting Jet Plumes. 10th Applied Aerodynamics Conference, Palo Alto, California June 1992.
  22. Jones, W. T. and Abdol-Hamid K. S.: Computational Analysis of Drag Reduction Techniques for Afterbody/Nozzle/Empennage Configurations. Aerospace Technology Conference and Exposition, Long Beach, California September 1992.
  23. Abdol-Hamid, K. S.; Uenishi, K.; Keith, B. D.; and Carlson, John R.: Commercial Turbofan Engine Exhaust Nozzle Flow Analyses. Journal of Propulsion and Power, Vol. 9, No. 3, May-June 1993.
  24. Carlson, John R.; and Abdol-Hamid, Khaled S.: Prediction of Static Performance for Single Expansion Ramp Nozzles. AIAA Paper No. 93-2571, AIAA/SAE/ASME/ASEE 29th Joint Propulsion Conference, June 28-30, 1993.
  25. Carlson, John R.; Abdol-Hamid, K. S.; and Pao, S. Paul: Computational Analysis of Vented Supersonic Exhaust Nozzle Using a Multiblock/Multizone Strategy. Journal of Propulsion and Power, (tentative) Vol. 9, No. 6, November-December 1993.
  26. Carlson, John R.: Analytic Prediction of Isolated Performance of an Axisymmetric Nozzle at M = 0.90. NASA TM-4506, 1993.Format(s): Postscript, or PDF
  27. Pao, S. P.; Carlson, J. R.; and Abdol-Hamid, K. S.: Computational Investigation of Circular-to-Rectangular Transition Ducts. Journal of Propulsion and Power, Volume 10, Number 1, January-February 1994, pp. 95-100.
  28. Carlson, J. R.; Computational Prediction of Isolated Performance of an Axisymmetric Nozzle at Mach Number 0.90. NASA TM-4506, February 1994.
  29. Kuhne, C. M.; Uenishi, K.; Leon, R. M.; Abdol-Hamid, K. S.; CFD Based 3D Aero Analysis System for High-Speed Mixer-Ejector Exhaust Nozzles. AIAA 94-2941, 30th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Indianapolis, IN, June 27-29, 1994.
  30. Giuliano, V. J.; Flugstad, T. H.; Semmes, R.; and Wing, D. J.: Static Investigation and Computational Fluid Dynamics (CFD) Analysis of Flowpath Cross-Section and Trailing-Edge Shape Variations in Two Multiaxis Thrust Vectoring Nozzle Concepts. AIAA 94-3367, 30th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Indianapolis, IN, June 27-29, 1994.
  31. Carlson, J. R.; and Asbury, S. C.: Two-Dimensional Converging-Diverging Rippled Nozzles at Transonic Speeds. NASA TP-3440, July 1994.
  32. Lakshmanan, B.; and Abdol-Hamid, K. S.: Investigation of Supersonic Jet Plumes Using an Improved Two-Equation Turbulence Model. Journal of Propulsion and Power, Volume 10, Number 5, September-October 1994, pp. 736-741.
  33. Alexander, Kristina L. : Investigation of a Supersonic Cruise Nozzle. 45th Annual Southern Region Student Conference, 1994. as a NASA Technical Paper
  34. Lakshmanan, B.; and Abdol-Hamid, K. S.: Investigation of Supersonic Jet Plumes Using an improved Two-Equation Turbulence Model. Journal of Propulsion and Power, Vol. 10, No. 5, September 1994.
  35. Lakshmanan, B.; Chylek, T.; and Tiwari, S. N.: Application of Nonlinear k-e Model to Supersonic Separated Flows. AIAA 95-0228, 33rd Aerospace Sciences Meeting and Exhibit, Reno, NV, January 9-12, 1995.
  36. Abdol-Hamid, K. S.; Lakshmanan, B.; and Carlson, J. R.: Application of Navier-Stokes Code PAB3D with k-e Turbulence Model to Attached and Separated Flows. NASA TP-3480, January 1995.
  37. Abdol-Hamid, K. S.; Carlson, J. R.; and Pao, S. P.: Calculation of Turbulent Flows Using Mesh Sequencing and Conservative Patch Algorithm. AIAA 95-2336, 31st AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, San Diego, CA, July 10-12, 1995
  38. J. F. Federspiel, L. S. Bangert, D. J. Wing and T. Hawkes, Fluidic Control of Nozzle Flow---Some Performance Measurements , 31st AIAA/ASME/SAE/ASEE Joint Propulsion Conference, San Diego, California, AIAA Paper No. 95-2605, July 10-12, 1995, 
  39. Carlson, J. R.; Pao, S. P.; Abdol-Hamid, K. S.; and Jones, W. T.: Aerodynamic Performance Predictions of Single and Twin Jet Afterbodies. AIAA 95-2622 , 31st AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, San Diego, CA, July 10-12, 1995.
  40. "Aerodynamics of 3-D Aircraft Afterbodies ", AGARD Advisory Report No. 318, September 1995.
  41. Abdol-Hamid, K. S.: Implementation of Algebraic Stress Models in a General 3-D Navier-Stokes Method (PAB3D). NASA CR-4702, December 1995.
  42. Deere, K. A.: An Experimental and Computational Investigation of a Translating Throat Single Expansion-Ramp Nozzle. Thesis for Master of Science for the George Washington University. December 1995.
  43. William B. Compton III, Comparison of Turbulence Models for Nozzle-Afterbody Flows With Propulsive Jets , NASA TP-3592, September 1996, pp. 117,  Format(s): Postscript, or PDF
  44. Capone, F. J.; Asbury S. C.; and Deere, K. A.: Experimental and Computational Induced Aerodynamics from Missile Jet Reaction Controls at Angles of Attack to 75 Degrees. AIAA 96-2479, 14th AIAA Applied Aerodynamics Conference, New Orleans, LA, June 18-20, 1996.
  45. Carlson, J. R.; Reubush D. E.: High Reynolds Number Analysis of an Axisymmetric Afterbody with Flow Separation. AIAA 96-2274, 19th AIAA Advanced Measurement and Ground Testing Technology Conference, New Orleans, LA, June 17-20, 1996.
  46. Deere, K. A.; and Asbury, S. C.: An Experimental and Computational Investigation of a Translating Throat Single Expansion-Ramp Nozzle.AIAA 96-2540 , 32nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Lake Buena Vista, FL, July 1-3, 1996.
  47. Midea, A. C.; Austin, T.; Pao, S. P.; DeBonis, J. R.; and Mani, M.: High Speed Civil Transport (HSCT) Isolated Nacelle Transonic Boattail Drag Study and Results Using Computational Fluid Dynamics (CFD). HSR025, February 1996.
  48. Carlson, J. R.: High Reynolds Number Analysis of Flat Plate and Separated Afterbody Flow Using Non-Linear Turbulence Models. AIAA 96-2544, 32nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Lake Buena Vista, Florida, Jult 1-3, 1996.
  49. Pao, S. Paul and Abdol-Hamid, K. S.: Numerical Simulation of Jet Aerodynamics Using Three-dimensional Navier-Stokes Method (PAB3D). NASA TP-3596, September 1996.
  50. Lakshmann, B.; Tiwari, S. and Abdol-Hamid, K.: Prediction of High Speed Free-Shear Flows Using High-Order Turbulence Models. AIAA 97-0762, 35th Aerospace Conference and Exhibit, Reno, NV, January 6-9, 1997.
  51. Hunter, C.: Experimental, Theoretical, and Computational Investigation of Separated Nozzle lows. AIAA 98-3107, 34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Cleveland, OH, July 13-15, 1998.
  52. Karen A. Deere, PAB3D Simulations of a Nozzle With Fluidic Injection for Yaw Thrust-Vector Control , 34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Cleveland, Ohio, AIAA 98-3254, July 13-15, 1998, pp. 12.
  53. John R. Carlson, Prediction of Very High Reynolds Number Compressible Skin Friction , 20th AIAA Advanced Measurement and Ground Testing Technology Conference, Albuquerque, New Mexico,AIAA 98-2880, June 15-18, 1998, (2MB).
  54. Qunzhen Wang, Steven J. Massey, Khaled S. Abdol-Hamid and Neal T. Frink, Solving Navier-Stokes Equations With Advanced Turbulence Models on Three-Dimensional Unstructured Grids , 37th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, AIAA 99-0156, January 11-14, 1999,  
  55. Deere, K. and Asburty, S.: Experimental and Computational Investigation of a Translating-Throat, Single-Expansion-Ramp Nozzle. NASA TP-1999-209138, May 1999.
  56. Hunter, Craig A. and Deere, Karen A. "Computational Investigation of Fluidic Counterflow Thrust Vectoring". AIAA 99-2669, presented at the 35th Annual AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Los Angeles, CA, June 20-23, 1999.
  57. Hunter, C. and Deere, K.:Experimental Investigation of Convoluted Contouring for Aircraft Afterbody Drag Reduction. 35th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit. AIAA 99-2670, June 1999
  58. Duquesne N.; Carlson,J.R.; Rumsey,C.L. and Gatski,T.B.: Computation of Turbulent Wake Flows in Variable Pressure Gradient, 30th AIAA Fluid Dynamics Conference, June 28 - July 1, 1999, Norfork, VA, AIAA 99-3781
  59. Deere, K. :Computational Investigation of the Aerodynamic Effects on Fluidic Thrust Vectoring. 36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit. AIAA 2000-3598, July 2000. Format(s):
  60. Carlson, J.R.; Duquesne, N.; Rumsey,C.L.; Gatski,T.B.: Computation of turbulent wake flows in variable pressure gradient. Computers & Fluids 30 (2001) 161-187.
  61. Kenrick, W.: An Experimental and Computational Investigation of Multiple Injection Ports in a Convergent-Divergent Nozzle for Fluidic Thrust Vectoring. Master degree Thesis, George Washington University, 2001
  62. Thomas, R. H.; Kinzie, K. W.; and Pao, S. P. :Computational Analysis of a Paylon-Cheveron Core Nozzle Interaction. 7th AIAA/CEAS Aeroacoustics Conference, Maastricht, The Netherlands, AIAA 2001-2185, May 28-30, 2001, pp. 12, (2.9MB PS, 1.7MB PDF).
  63. Massey, S.; and Kenrick, W.: Computational Analyses of Propulsion Aeroacoustics for Mixed Flow Nozzle Pylon Installation at TakeoffEagle Aeronautics, Inc. and Analytical Services and Materials, Inc., NASA/CR-2001-211056, September 2001, pp. 35
  64. Capone, F. J and Deere, K. :Transonic Investigation of Two-Dimensional Nozzles Designed for Supersonic Cruise. AIAA 2001-3199, 37th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, July 2001.
  65. Walter M. Presz, Jr., Gary Reynolds and Craig Hunter :Thrust Augmentation With Mixer/Ejector Systems. 40th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, AIAA 2002-0230, January 14-17, 2002, pp. 11.
  66. Karen A. Deere and Mohagna J. Pandya :Propulsion Simulations With the Unstructured-Grid CFD Tool, TetrUSS, 32nd AIAA Fluid Dynamics Conference and Exhibit, St. Louis, Missouri, AIAA 2002-2980, June 24-26, 2002.
  67. Massey, S. and Abdol-Hamid, K., "Enhancement and Validation of PAB3D for Unsteady Aerodynamics", AIAA 2003-1235, Reno, NV, January 2003.
  68. Abdol-Hamid, K., Massey, S. and Caldwell, S. “Unified Process Management System for Computational Fluid Dynamics (UPMS)”, AIAA Paper 2003-0803, Reno, NV, January 2003
  69. J. R. Carlson. “Applications of Algebraic Reynolds Stress Turbulence Models Part 1: Incompressible Flat Plate.” AIAA Journal of Propulsion and Power, Vol. 13, No. 5, pp. 610-619, September-October 1997.
  70. J. R. Carlson. “Applications of Algebraic Reynolds Stress Turbulence Models Part 1: Transonic Shock-Separated Afterbody.” AIAA Journal of Propulsion and Power, Vol. 13, No. 5, pp. 620-628, September-October 1997.
  71. Craig Allen Hunter, “An Approximate Jet Noise Prediction Method Based on Reynolds-Averaged Naviar-Stokes Computational Fluid Dynamics Simulation.” Ph.D. Thesis, George Washington University, January 2002
  72. Hunter, C., Pao, S. and  Thomas, R., “Development of a Jet Noise Prediction Method for Installed Jet Configurations,” 9th AIAA/CEAS Aeroacoustics Conference and Exhibit, May 12-14, 2003, Hilton Head, South Carolina. AIAA 2003-3169.
  73. Massey, S.J., Thomas, R.H., Abdol-Hamid, K.S., and Elmiligui, A., “Computational and Experimental Flowfield Analyses of Separate Flow Chevron Nozzles and Pylon Interaction,” 9th AIAA/CEAS Aeroacoustics Conference and Exhibit, May 12-14, 2003, Hilton Head, South Carolina. AIAA-2003-3212.
  74. Abdol-Hamid, Pao, S, Massey, S.J., and Elmiligui, A., “Temperature Corrected Turbulence Model for High Temperature Jet Flow.” AIAA-2003-4070.
  75. Berrier, B. L.; Hamid, K. S.; and Massey, S. J. “Wind Tunnel Investigation of Spanwise Blowing for Control of an Advanced Aircraft Configuration.” NASA TP-2003-212409, July 2003, 71 p.
  76. Elmiligui, A., Hamid, K. S., Massey, S.J., and Pao, S.“A Numerical Study of Flow Past a Circular Cylinder Using RANS, Hybrid RANS/LES and PANS Formulations”AIAA 2004-4959
  77. Hunter, C., Thomas, R.H., Abdol-Hamid, K., Pao, P. S., Elmiligui, A., Massey, S., "Computational Analysis of the Flow and Acoustic Effects of Jet-Pylon Interaction." 11th AIAA/CEAS Aeroacoustics Conference. 23-25 May 2005, Monterey, California. AIAA 2005-3083
  78. Abdol-Hamid, K., and Elmiligui, A., "Numerical Study of High Temperature Jet Flow Using RANS/LES and PANS Formulations." 23rd AIAA Applied Aerodynamics Conference. 6-9 June 2005, Toronto Canada. AIAA Paper 2005-5092.
  79. K. Deere, B. Berrier, J. Flamm, and S. Johnson, "A Computational Study of a Dual Throat Fluidic Thrust Vectoring Nozzle Concept"  41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 10-13 Jul 2005, Tucson, Arizona. AIAA Paper 2005-3502
  80. J. Flamm, K. Deere, B. Berrier, S. Johnson and M. Mason. "Experimental Study of a Dual-Throat Fluidic Thrust-Vectoring Nozzle Concept."  41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 10-13 Jul 2005, Tucson, Arizona. AIAA Paper 2005-3503.
  81. Elmiligui, A., Abdol-Hamid, K., and Hunter, C., "Numerical Investigation Flow in an Over-expanded Nozzle with Porous Surfaces." 41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 10-13 Jul 2005, Tucson, Arizona. AIAA Paper 2005-4159

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