Shock interference heat transfer to tank configurations mated to a straight-wing space shuttle orbiter at Mach number 10.3 / Davis H. Crawford ; Langley Research Center, Hampton, Va.

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Bibliographic Details
Online Access:	Search for the full-text version of this title in HathiTrust
Main Author:	Crawford, Davis H.
Corporate Authors:	Langley Research Center, United States. National Aeronautics and Space Administration
Format:	Government Document Book
Language:	English
Published:	Washington : Springfield, Va. : National Aeronautics and Space Administration ; For sale by the National Technical Information Service, 1976.
Series:	NASA technical note ; D-8203.
Subjects:	Heat > Transmission. Space vehicles. Aerothermodynamics.

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Holdings details from Norlin Library - Government Information - US
Call Number:	NAS 1.14:D-8203
NAS 1.14:D-8203	Available Place a Hold