Flow-thermal-structural study of aerodynamically heated leading edges
Author:
Affiliation:
1. NASA, Langley Research Center, Hampton, VA
2. Old Dominion University, Norfolk, VA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1988-2245
Reference21 articles.
1. Verification tests of durable thermal protection system concepts
2. Analysis of aerothermal loads on spherical dome protuberances
3. Finite element prediction of aerothermal-structural interaction of aerodynamically heated panels
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