Using Pressure- and Temperature-Sensitive Paint on the Aftbody of a Capsule Entry Vehicle
Author:
Affiliation:
1. NASA Langley Research Center, Hampton, Virginia 23681
2. ATK Aerospace Company, Hampton, Virginia 23681
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.37258
Reference34 articles.
1. Luminescent barometry in wind tunnels
2. Pressure-sensitive paint in aerodynamic testing
3. Temperature- and Pressure-Sensitive Luminescent Paints in Aerodynamics
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