Effect of wing sweep, angle of attack, Reynolds number, and wing root fillet on the interference heating to the wing windward surface of an entry vehicle configuration / by Louis E. Clark.

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Main Author: Clark, Louis E. (Author)
Format: Government Document eBook
Language:English
Published: Washington, D.C. : National Aeronautics and Space Administration, December 1972.
Series:NASA technical note ; D-7060.
Subjects:

MARC

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