Pressure-Sensitive Paint Measurements on the NASA Common Research Model in the NASA 11-ft Transonic Wind Tunnel
Author:
Affiliation:
1. NASA Ames Research Center
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2011-1128
Reference23 articles.
1. Temperature- and Pressure-Sensitive Luminescent Paints in Aerodynamics
2. SURFACE PRESSURE MEASUREMENTS USING LUMINESCENT COATINGS
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