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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Bibliographic Details
Online Access:	Online Access Search for the full-text version of this title in HathiTrust
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:	Space vehicles > Atmospheric entry. Leading edges (Aerodynamics) Aerodynamic heating. Aerothermodynamics. Space shuttles. Aerospace vehicles. Aerodynamics.

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Holdings details from Norlin Library - Government Information - US
Call Number:	NAS 1.14:D-7060
NAS 1.14:D-7060	Available Place a Hold