Wind Tunnel Measurements of Shuttle Orbiter Global Heating With Comparison to Flight
Author:
Affiliation:
1. NASA Langley Research Center
2. George Washington University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2002-4701
Reference21 articles.
1. Infrared Sensing Aeroheating Flight Experiment: STS-96 Flight Results
2. Shuttle Orbiter Fuselage Global Temperature Measurements from Infrared Images at Hypersonic Speeds
3. Reduction and analysis of phosphor thermography data with the IHEAT software package
4. Miller, C. G. "Langley Hypersonic Aerodynamic/ Aerothermodynamic Testing Capabilities - Present and Future," AIAA Paper 90-1376,June1990.
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