Aerodynamic database development for the Hyper-X airframe integrated scramjet propulsion experiments

18th Applied Aerodynamics Conference

Volumn , Issue , 2000, Pages

  Engelund, Walter C ^a   Holland, Scott D ^a   Cockreli Jr , Charles E ^a   Bittner, Robert D ^b  

^a NASA LANGLEY RESEARCH CENTER   (United States)

^b FDC/NYMA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMIC STABILITY; AERODYNAMICS; AIRFRAMES; COMPUTATIONAL FLUID DYNAMICS; DATABASE SYSTEMS; ENGINES; FLIGHT CONTROL SYSTEMS; NASA; PROPULSION; ROCKETS; SOFTWARE TESTING; STRUCTURAL FRAMES; TESTING; WIND TUNNELS;

AERODYNAMIC DATABASE; FLIGHT EXPERIMENTS; INDIRECT EFFECTS; RESEARCH VEHICLES; SCRAMJET ENGINES; SCRAMJET PROPULSION; STABILITY AND CONTROL; WIND TUNNEL TESTS;

RAMJET ENGINES;

EID: 85087596159     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2000-4006     Document Type: Conference Paper

References (24)

1. Rausch, V. L., McClinton, C. R., Hicks, J. W.: "NASA Scramjet Flight to Breath New Life into Hypersonics," Aerospace America, July 1997.
2. Schweikart, L.: The Hypersonic Revolution: Case Studies in the History of Hypersonic Technology. Volume III-The Quest for the Orbital Jet: The National A ero-Space Plane Program (1983 - 1995). Air Force History and Museums Program, Bolling AFB, D. C., 1998.
3. Scramjet Propulsion (Chapter 5, Appendix B: NASA's Hyper-X Program), Edited by Dr. T. Curran and Dr. S.N.B. Murthy, AIAA Progress In Astronautics and Aeronautics Series, Vol. TBD, 2000.
4. Rausch, V. L., McClinton, C. R., Crawford, L.: "Hyper-X: Flight Validation of Hypersonic Airbreathing Technology," ISABE Paper 97-7024, Sept. 1997.
5. McClinton, C. R: "Hyper-X Propulsion," University of Tennessee Space Institute Hypersonics Short Course notes, April, 2000.
6. Hunt, J. L., Eiswirth, E. A. "NASA's Dual-Fuel Airbreathing Hypersonic Vehicle Study," AIAA CP-96-4591, Presented at the 7th International Space Planes and Hypersonics Systems & Technology Conference, Nov. 1996.
7. Bogar, T. J., Alberico, J. F., Johnson, D. B., Espinosa, A. M., Lockwood, M. K.: "Dual-Fuel Lifting Body Configuration Development," AIAA CP 96-4592, Presented at the 7th International Space Planes and Hypersonics Systems & Technology Conference, Nov. 1996.
8. Air Launched Flight Experiment Final Report. McDonnell Douglas Aerospace, June 1995.
9. Voland, R. T., Rock, K. E., Huebner, L. D., Witte, W Fisher, K. E., and McClinton, C. R.: "Hyper-X Engine Design and Ground Test Program," AIAA 98-1532, Presented at the 8lh International Space Planes and Hypersonics Systems & Technology Conference, April 1998, Norfolk, VA.
10. Reubush, D. E.: "Hyper-X Stage Separation-Background and Status," AIAA 99-4818, Presented at the AIAA 9th International Space Planes and Hypersonic Systems and Technologies Conference, Norfolk, Virginia, Nov. 1999.
11. McClinton, C. R., Voland, R. T., Holland, S. D., Engelund, W. C., White, J. T., Pahie, J. W.: "Wind Tunnel Testing, Flight Scaling and Flight Validation with Hyper-X," AIAA 98-2866, presented at the 20th AIAA Advanced Measurement and Ground Testing Technology Conference, June 1998, Albuquerque, NM.
12. Huebner, L. D., Rock, K. E., Witte, D. W., Ruf, E. G., and Andrews, E. H, Jr.: "Hyper-X Engine Testing in the NASA Langley 8-Foot High Temperature Tunnel." AIAA 2000-3605, presented at the 36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Huntsville, AL, July, 2000.
13. Rovner, D.: "GN&C for Pegasus Air Launched Space Booster: Design and First Flight Results," AIAA CP 91-1105, 1991
14. Allen, V.: "Hyper-X Launch Vehicle Aerodynamics Development," AIAA 2000-4007, Presented at the 18th AIAA Applied Aerodynamics Conference, Denver, CO, Aug., 2000.
15. Woods, W. C., Holland, S. D.: "Hyper-X Stage Separation Wind Tunnel Test Program," AIAA 2000-4008, Presented at the 18th AIAA Applied Aerodynamics Conference, Denver, CO, Aug., 2000.
16. Buning, P. G., Wong, T. C., Dilley, A. D., and Pao, J. L.: "Prediction of Hyper-X Stage Separation Aerodynamics using CFD," AIAA 2000-4009, Presented at the 18* AIAA Applied Aerodynamics Conference, Denver, CO, Aug., 2000.
17. Heiser, W. H., and Pratt, D. T.: Hypersonic Airbreathing Propulsion, AIAA Education Series, AIAA, Inc., Washington, D. C., 1994.
18. Holland, S. D., Woods, W. C and Engelund, W. C.: "Hyper-X Research Vehicle (HXRV) Experimental Aerodynamics Test Program Overview," AIAA-2000-4011, Presented at the 18th AIAA Applied Aerodynamics Conference, Denver, CO, Aug., 2000.
19. Huebner, L. D., and Tatum, K. E.: "CFD Code Calibration and Inlet-Fairing Effects on a 3D Hypersonic Powered-Simulation Model," AIAA 933041, July 1993.
20. Cockrell, C. E., Jr., Engelund, W. C., Bittner, R. D., Dilley, A. D., Jentink, T. N., and Frendi, A.: " Integrated Aero-Propulsive CFD Methodology for the Hyper-X Flight Experiment," AIAA-2000-4010, Presented at the 18th AIAA Applied Aerodynamics Conference, Denver, CO, Aug., 2000.
21. Berry, S. A., Auslander A. H., and Dilley, A. D.: "Hypersonic Boundary Layer Trip Development for Hyper-X," AIAA-2000-4012, Presented at the 18th AIAA Applied Aerodynamics Conference, Denver, CO, Aug., 2000.
22. White, J. T.: "X-43A Real Time Angle-of-Attack Estimation Scheme Utilizing Flush Airdata Sensing (FADS) System Inputs," AIAA-2000-4013, Presented at the 18Ih AIAA Applied Aerodynamics Conference, Denver, CO, Aug., 2000.
23. Morelli, E., and Klein, V., "Optimal Input Design for Aircraft Parameter Estimation Using Dynamic Programming Principles," AIAA 90-2801, Aug. 1990.
24. Illif, K. W, Maine, R. E., and Montgomery, T. D., "Important Factors in the Maximum Likelihood Analysis of Flight Test Maneuvers," NASA TP 1459, Jan. 1979.