Using Pressure- and Temperature-Sensitive Paint for Global Surface Pressure and Temperature Measurements on the Aft-Body of a Capsule Entry Vehicle
Author:
Affiliation:
1. NASA Langley Research Center
2. ATK
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2008-1230
Reference30 articles.
1. Experimental Measurement of RCS Jet Interaction Effects on a Capsule Entry Vehicle
2. Luminescent barometry in wind tunnels
3. Aerodynamic measurements based on photoluminescence
4. Pressure-sensitive paint in aerodynamic testing
5. Temperature- and Pressure-Sensitive Luminescent Paints in Aerodynamics
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