Effect of Temperature-Sensitive-Paint Thickness on Global Heat Transfer Measurement in Hypersonic Flow
Author:
Affiliation:
1. Tohoku University, Sendai 980-8579, Japan
2. Japan Aerospace Exploration Agency, Tokyo 182-8522, Japan
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Condensed Matter Physics,Aerospace Engineering,Space and Planetary Science,Fluid Flow and Transfer Processes,Mechanical Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.34152
Reference18 articles.
1. Reduction of data from thin-film heat-transfer gages - A concise numerical technique.
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