Pressure-sensitive paint measurements on aeroelastic wings in transonic flow
Author:
Affiliation:
1. NASA, Ames Research Center, Moffett Field, CA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1997-389
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4. Submillisecond response times of oxygen‐quenched luminescent coatings
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2. Measurement Technology for use in Active Flow Control;22nd AIAA Aerodynamic Measurement Technology and Ground Testing Conference;2002-06-24
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