Calibration of the langley 8-foot high temperature tunnel for hypersonic airbreathing propulsion testing

Advanced Measurement and Ground Testing Conference

Volumn , Issue , 1996, Pages

  Huebner, Lawrence D ^a   Rock, Kenneth E ^a   Voland, Randall T ^a   Wieting, Allan R ^a  

^a NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; CALIBRATION; ENTHALPY; MACH NUMBER; NASA;

AEROTHERMAL LOADS; AIR-BREATHING PROPULSION; FLOW CHARAC-TERISTICS; HIGH TEMPERATURE; PROPULSION SYSTEM; STRUCTURAL VERIFICATION; TUNNEL FLOW QUALITY;

PROPULSION;

EID: 84983121010     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1996-2197     Document Type: Conference Paper

References (6)

1. Howell, R. R.; and Hunt, L. R.: "Methane-Air Combustion Gases as an Aerodynamic Test Medium. “Journal of Spacecraft, Vol. 9, No. 1, January 1972, pp. 7-12.
2. Reubush, D. E.; Puster, R. L.; and Kelly, H. N.: "Modification to the Langley 8-Foot High Temperature Tunnel for Hypersonic Propulsion Testing, “AIAA Paper 87-1887, June 1987.
3. Phelps, D. C.; McVey, W. J.; and Faulkner, R. F.: National Aerospace Plane Concept Demonstration Engine Final Test Report (U). NASP Report X30SP94007, January 1995. (SECRET)
4. Erickson, W. D.; Hall, G. H.; and Prabhu, R. K.: Finite-Rate Water Condensation in Combustion-Heated Wind Tunnels. NASA TN-2833, 1988.
5. Perrell, E. R.: Computation of Combustion Heated Hypersonic Wind Tunnel Flows in Phase Nonequilibrium, Ph. D. Thesis, North Carolina State University, 1994.
6. McBride, B. J.; Heimel, S.; Ehlers J. G.; and Gordon, S.: Thermodynamic Properties to 6000° K for 210 Substances Involving the First 18 Elements. NASA SP-3001, 1963.