Hyper-X wind ttinnel program

36th AIAA Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 1998, Pages

  McClinton, C R ^a   Holland, S D ^a   Rock, K E ^a   Engelund, W C ^a   Voland, R T ^a   Huebner, L D ^a   Rogers, R C ^a  

^a NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE ENGINEERING; AIRFRAMES; COMBUSTION; NASA; NUMERICAL METHODS; PROPULSION; SOFTWARE TESTING; STRUCTURAL FRAMES; UNMANNED VEHICLES; VEHICLES; WIND TUNNELS;

AIR BREATHING VEHICLES; EXPERIMENTAL PROGRAM; HYPERSONIC TECHNOLOGY; LABORATORY ENVIRONMENT; PERFORMANCE VALIDATION; PROTOTYPE DEVELOPMENT; SUPERSONIC COMBUSTION; VERIFICATION-AND-VALIDATION;

SUPERSONIC AIRCRAFT;

EID: 84983127068     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (26)

1. James L. Hunt, Charles R. McClinton; Scramjet Engine/Airframe Integration Methodology. AGARD Conference, Palaiseau, France, April 14-16, 1997.
2. Becker, J. V. and Baals, D. D.: The aerodynamic Effects of Heat and Compressibility in the Internal Flow Systems of Aircraft. NACA ACR, Sept. 1942; also NACA TR 773.
3. Guy, R. W., Rogers, R. C, Pulster, R. L., Rock, K. E., and Diskin, G. S.: The NASA Langley Scramjet Test Complex, AIAA 96-3243, 32nd AIAA / ASME/SAE/ASEE Joint Propulsion Conference, July 1-3, 1996, Lake Buena Vista, EL.
4. Andrews, E. H.; and Mackley, E. A.: NASA's Hypersonic Research Engine Project -A Review. NASA TM 107759, Oct. 1994.
5. Anderson, G. Y., Bencze, D. P. and Sanders, B. W.: "Ground tests confirm the promise of hypersonic propulsion" Aerospace America V25 No. 9, pp 38-42, Sept. 1987.
6. Guy, R. W.; and Mackley, E. A.: Initial Wind Tunnel Tests at Mach 4 and 7 of a Hydrogen-Burning, AirFrame-Integrated Scramjet AIAA paper 79-8045, presented at 4th International Symposium on Air Breathing Engines, April 1-6, 1979.
7. Stalker, R. J., Simmons, A. P., Mee, D. J.: Measurement of Scramjet Thrust in Shock Tunnels. 18th AIAA Aerospace Ground Testing Conference. AIAA 94-2516, June 1994, Colorado Springs, CO.
8. Vincent L. Rausch, Charles R. McClinton, and J. Larry Crawford: Hyper-X: Flight Validation of Hypersonic Airbreathing Technology, ISABE 97-7024, Sept. 7-12, 1997, Chattanooga, TN.
9. Henry, J. R. and Anderson, G. Y.: Design Considerations for the Airframe-Integrated Scramjet. Presented at the 1st International Symposium on Air Breathing Engines, Marseilles, France, June 1972 (also, NASA TM X-2895, 1973).
10. Vincent L. Rausch, Charles R. McClinton and John W. Hicks: NASA Scramjet Flights to Breath New Life into Hypersonics, Aerospace America, July 1997.
11. Iliff, K. W. and Shafer, M. F.: Extraction of Stability and Control Derivatives from Orbiter Flight Data. NASA CP 3248, April 1995.
12. Morelli, E. A.: Flight Test Validation of Optimal input Design and Comparison to Conventional Inputs. AIAA 97-3711, AIAA Atmospheric Flight Mechanics Conference, Aug. 11-13, 1997. New Orleans, LA.
13. Miller, C. G., IE, "Langley Hypersonic Aerodynam-ic/Aerothermodynamic Testing Capabilities -Present and Future," AIAA CP-90-1376, AIAA 16th Aerodynamic Ground Testing Conference, June 1990.
14. Pirrello C. J. et. al.: An inventory of Aeronautical Ground Research Facilities. Vol. 1 -Wind Tunnels. NASA CR 1874, Prepared by McDonnell Aircraft Co., Nov. 1971.
15. Penaranda. F. E., and Freda, M. S., "Aeronautical Facilities Catalogue, Vol. 1 -Wind Tunnels," NASA RP-1132, Jan. 1985.
16. Bums, K., Deters, K., Haley, C. P., and Kihlken, T.: "Viscous Effects on Complex Configurations -Final Report," WL-TR-95-3059, August, 1995.
17. Bonner, E., Clever, W., and Dunn, K.: "Aerodynamic Preliminary Analysis System n, Part I -Theory," 1989.
18. Godfrey, A. G., " GASP Version 3 User's Manual," Aerosoft, Inc., May 1996.
19. Neal T. Fink, Shahyar Pirzadeh and Paresh C. Parikh. An Unstructured-Grid Software System for Solving Complex Aerodynamic Problems. Workshop on Surface Modeling, Grid Generation and Related Issues on CFD, Cleveland, Ohio, May 9-11, 1995. NASA CP 3291, pp. 289-308.
20. Lohner, R.; Three-Dimensional Fluid-Structure Interaction using a Finite Element Solver and Adaptive Remeshing. Computing Systems in Engineering, Vol. 1, 1990, pp 257-272.
21. Emami, S.; Trexler, C. A.; Auslander, A. H. and Wei-dner, J. P.: Experimental Investigation of Inlet-Com-bustor Isolators for a Duel-Mode Scramjet at a Mach Number of 4. NASA Technical Paper 3502, May 1995.
22. G. Roffe, RJ. Bakos, J. I. Erdos and W. Swartwout. The Propulsion Test Complex at GASL. IS ABE 97-7096, Sept. 1997.
23. Huebner, L. D., Rock, K. E., Voland, R. T., Wiet-ing, A. R., "Calibration of the Langley 8-Foot High Temperature Tunnel for Hypersonic Airbreathing Propulsion Testing," AIAA CP-96-2197, 19th AIAA Advanced Measurement and Ground Testing Technology Conference, June 1996.
24. Bakos, R. J.; Castrogiovanni, J. F.; Calleja, J. F.; Nucci, L. and Erdos, J. I.: Expansion of the Scramjet Ground Test Envelope of the HYPULSE Facility. AIAA 96-45006, AIAA 7th International Space Planes and Hypersonic Systems and Technology Conference, Norfolk, VA, Nov. 1996.
25. Rogers, R. C.; Weidner, E. H.; and Bittner, R. D.: Quantification of Scramjet Mixing in Hypervelocity Flow of a Pulse Facility. AIAA 94-2518, June 1994.
26. Wang, Liang-Guo; Trucco, R. E.; Sachse G. W.; Campbell, R. E.; and Davis, R. E.: Water Vapor Measurements for Combustion Diagnostics Using a 1350 nm Tunable Diode Laser. Presented at SPIE's OE/LASE '94, Jan. 22-29, 1994, Los Angeles, CA.