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Available items only
Pittman, Jimmy L., author.
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.
[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, December 1980.
Connect to http://purl.fdlp.gov/GPO/gpo71373
Axe Federal Documents Online
1 online resource (113 pages) : illustrations.
text txt rdacontent
computer c rdamedia
online resource cr rdacarrier
NASA technical paper ; 1767
NASA technical paper ; 1767.
Title from title screen (viewed on Aug. 19, 2016).
"Performing Organization: NASA Langley Research Center"--Report documentation page.
Includes bibliographical references (pages 14-15).
Type Of Report
National Aeronautics and Space Administration 505-31-73-01 L-13868
Supersonic wind tunnels.
Aerodynamics, Supersonic. (OCoLC)fst00798221
Hypersonic planes. (OCoLC)fst00965814
Mach number. (OCoLC)fst01004756
Supersonic wind tunnels. (OCoLC)fst01139019
Angle of attack.
Electronic government information.
Riebe, Gregory D., author.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, issuing body.
Print version: Pittman, Jimmy L. Experimental and theoretical aerodynamic characteristics of two hypersonic cruise aircraft concepts at Mach numbers of 2.96, 3.96, and 4.63 (OCoLC)7325143
Microfiche version: Pittman, Jimmy L. Experimental and theoretical aerodynamic characteristics of two hypersonic cruise aircraft concepts at Mach numbers of 2.96, 3.96, and 4.63 (OCoLC)711544698
Gpo Item No.
Available items only