Hyper-X engine design and ground test program

8th AIAA International Space Planes and Hypersonic Systems and Technologies Conference

Volumn , Issue , 1998, Pages 1-12

  Voland, R T ^a   Rock, K E ^a   Huebner, L D ^a   Witte, D W ^a   Fischer, K E ^a   McClinton, C R ^a  

^a NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COMBUSTION; ENGINES; FLIGHT CONTROL SYSTEMS; HYPERSONIC VEHICLES; MACHINE DESIGN; NASA; NUMERICAL METHODS; PROPULSION; RAMJET ENGINES; SUPERSONIC AIRCRAFT; WIND TUNNELS;

AIR BREATHING VEHICLES; HYPERSONIC TECHNOLOGY; LABORATORY ENVIRONMENT; PERFORMANCE VALIDATION; PERFORMANCE VERIFICATION; RISK REDUCTION EFFORTS; SUPERSONIC COMBUSTION; VERIFICATION-AND-VALIDATION;

SOFTWARE TESTING;

EID: 84983121734     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1998-1532     Document Type: Conference Paper

References (15)

1. Hunt, J. L.; and McClinton, C. R.: Scramjet Engine/Airframe Integration Methodology. AGARD Conference, Palaiseau, France, April 14-16, 1997.
2. Decker, 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. nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference, July 1-3, 1996, Lake Buena Vista, FL.
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, vol. 25, 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 79-8045, presented at 4th International Symposium on Air Breathing Engines, April 1-6, 1979.
7. Stalker, R. J.; Simmons, A. P.; and Mee, D. J.: Measurement of Scramjet Thrust in Shock Tunnels. AIAA 94-2516, 18th AIAA Aerospace Ground Testing Conference, June 1994, Colorado Springs, CO.
8. Rausch, V. L.; McClinton, C. R.; and Crawford, J. L.: 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. Rausch, V. L.; McClinton, C. R.; and Hicks, J. W.: NASA Scramjet Flights to Breathe New Life into Hypersonics. Aerospace America, vol. 35, No. 7, pp. 40-46, 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. McClinton, C. R.; Holland, S. D.; Rock, K. E.; Engelund, W. C.; Voland, R. T.; Huebner, L. D.; and Rogers, R. C.: Hyper-X Wind Tunnel Program. AIAA 98-0553, 36th AIAA Aerospace Sciences Meeting and Exhibit, January 12-15, 1998, Reno, NV.
14. Huebner, L. D.; Rock, K. E.; Voland, R. T.; and Wieting, 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.
15. Roffe, G.; Bakos, R. J.; Erdos, J. I.; and Swartwout, W.: The Propulsion Test Complex at GASL. ISABE 97-7096, Sept. 1997.