Free-flight investigation of a rocket-propelled model to determine the aerodynamic heating on a thin, unswept, untapered, multispar, aluminum-alloy wing at Mach numbers up to 2.22 / by Emily W. Stephens.

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Bibliographic Details
Main Author:	Stephens, Emily W.
Corporate Authors:	United States. National Aeronautics and Space Administration, Langley Research Center
Format:	Government Document Book
Language:	English
Published:	Washington [D.C.] : National Aeronautics and Space Administration, [1959]
Series:	NASA memorandum ; 12-15-58L.
Subjects:	Aerodynamic heating > Testing. Heat > Transmission > Testing. Aerodynamics, Supersonic > Testing.

Norlin Library - Government Information - US

Holdings details from Norlin Library - Government Information - US
Call Number:	NAS 1.10:12-15-58 L
NAS 1.10:12-15-58 L	Available Place a Hold