Experimental and theoretical aerodynamic characteristics of two hypersonic cruise aircraft concepts at Mach numbers of 2.96, 3.96, and 4.63 / Jimmy L. Pittman and Gregory D. Riebe.
- Physical Description: 1 online resource (113 pages) : illustrations.
- Publisher: [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, December 1980.
Title from title screen (viewed on Aug. 19, 2016).
"Performing Organization: NASA Langley Research Center"--Report documentation page.
|Bibliography, etc. Note:||
Includes bibliographical references (pages 14-15).
|Type of Report and Period Covered Note:||
|Funding Information Note:||
National Aeronautics and Space Administration 505-31-73-01 L-13868
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