PSP Measurement of a High-Lift-Device Model in JAXA 6.5m×5.5m Low-Speed Wind Tunnel
Author:
Affiliation:
1. Japan Aerospace Exploration Agency
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2007-1065
Reference19 articles.
1. SURFACE PRESSURE MEASUREMENTS USING LUMINESCENT COATINGS
2. Liu, T., Campbell, B. T., Burns, S. P. and Sullivan, J. P. Temperature- and Pressure-Sensitive Luminescent Paints in Aerodynamics.Appl.Mech. Rev., 50-4, 1997,pp.227-246.
3. Temperature Correction of Pressure-Sensitive Paint for Industrial Wind Tunnel Testing
4. Practical pressure-sensitive paint measurement system for industrial wind tunnels at JAXA
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