Cover image for Application of supersonic linear theory and hypersonic impact methods to three nonslender hypersonic airplane concepts at mach numbers from 1.10 to 2.86
Title:
Application of supersonic linear theory and hypersonic impact methods to three nonslender hypersonic airplane concepts at mach numbers from 1.10 to 2.86
Author:
Pittman, Jimmy L.
Personal Author:
Publication Information:
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va.] : [For sale by the National Technical Information Service], 1979.
Physical Description:
56 pages : illustrations ; 27 cm.
General Note:
"Langley Research Center."

"December 1979"--Cover.

Subject Category 02.
Language:
English
Format :
Book

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TL521.3 .T4 NOS.1535-1545 NO. 1539 Adult Non-Fiction Central Closed Stacks-Non circulating
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