Temperature Correction of Pressure-Sensitive Paint for Industrial Wind Tunnel Testing
Author:
Affiliation:
1. Institute of Aerospace Technology, Japan Aerospace Exploration Agency, Chofu, Tokyo 182-8522, Japan
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.13608
Reference9 articles.
1. Rapid technology assessment via unified deployment of global optical and virtual diagnostics
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3. Treating temperature-sensitivity effects of pressure-sensitive paint measurements
4. Blowdown tunnel application of pressure sensitive paint
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