Pressure and heat-transfer distributions in a simulated wing-elevon cove with variable leakage at a free-stream Mach number of 6.9
Author:
Affiliation:
1. NASA, Langley Research Center, Structures and Dynamics Div., Hampton, Va.
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1978-39
Reference9 articles.
1. Shuttle elevon cove aerodynamic heating by internal flow
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