Wind-tunnel investigation at mach numbers from 0.40 to 1.14 of the static aerodynamic characteristics of a nonlifting vehicle suitable for reentry / by Albin O. Pearson.

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Bibliographic Details
Main Author:	Pearson, Albin O.
Corporate Authors:	Langley Research Center, United States. National Aeronautics and Space Administration
Format:	Government Document Book
Language:	English
Published:	Washington [D.C.] : National Aeronautics and Space Administration, [1959]
Series:	NASA memorandum ; 4-13-59L.
Subjects:	Stability of space vehicles > Testing. Space vehicles > Atmospheric entry > Testing. Aerodynamics, Supersonic > Testing. Wind tunnel testing.

Norlin Library - Government Information - US

Holdings details from Norlin Library - Government Information - US
Call Number:	NAS 1.10:4-13-59 L
NAS 1.10:4-13-59 L	Available Place a Hold