Simultaneous global pressure and temperature measurement technique for hypersonic wind tunnels

21st Aerodynamic Measurement Technology and Ground Testing Conference

Volumn , Issue , 2000, Pages

  Buck, Gregory M ^a  

^a NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; AUTOMOBILE MANUFACTURE; COATINGS; HYPERSONIC VEHICLES; TEMPERATURE MEASUREMENT; THERMODYNAMICS;

ADVANCED MODELING; EXPERIMENTAL AERODYNAMICS; FEASIBILITY STUDIES; HYPERSONIC WIND TUNNELS; LANGLEY RESEARCH CENTERS; LUMINESCENT COATINGS; MEASUREMENT TECHNIQUES; PRESSURE AND TEMPERATURE;

WIND TUNNELS;

EID: 85088722239     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2000-2649     Document Type: Conference Paper

References (8)

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2. Buck, G. M. Surface Temperature/Heat Transfer Measurement Using a Quantitative Phosphor Thermography System, AIAA Paper 91-0064. January 1991.
3. Buck G. M. Simultaneous Luminescence Pressure and Temperature Measurement System for Hypersonic Wind Tunnels. Journal of Spacecraft and Rockets, Vol. 32. No. 5, September-October 1995, pp. 791-794.
4. Buck G. M. Rapid Model Fabrication and Testing for Aerospace Vehicles, AIAA Paper 2000-0826, January 2000.
5. Horvath T J., Berry, S. A., Merski, N. R., and Fitzgerald, S. M., X-38 Experimental Aerothermodynamics, AIAA Paper 2000-2685, June 2000.
6. Liu T., Campbell, B. T., Burns, S. P., and Sullivan, J. P., Temperature-and Pressure-Sensitive Luminescent Paints in Aerodynamics, Applied Mechanics Reviews, Vol. 50, No. 4, April 1997, pp. 227-246.
7. Merski N. R. Global Aeroheating Wind-Tunnel Measurements Using Improved Two-Color Phosphor Thermography Method, Journal of Spacecraft and Rockets, Vol. 36, No. 2, 1999, pp. 160-170.
8. Micol, J. R. Langley Aerothermodynamic Facilities Complex: Enhancements and Testing Capabilities, AIAA Paper 98-0147. January 1998.