Experimental and theoretical aerodynamic characteristics of two hypersonic cruise aircraft concepts at Mach numbers of 2.96, 3.96, and 4.63 /

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Bibliographic Details
Author / Creator:Pittman, Jimmy L., author.
Imprint:[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, December 1980.
Description:1 online resource (113 pages) : illustrations.
Language:English
Series:NASA technical paper ; 1767
NASA technical paper ; 1767.
Subject:
Format: E-Resource U.S. Federal Government Document Book
URL for this record:http://pi.lib.uchicago.edu/1001/cat/bib/10914244
Hidden Bibliographic Details
Other authors / contributors:Riebe, Gregory D., author.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, issuing body.
Notes:Title from title screen (viewed on Aug. 19, 2016).
"December 1980."
"Performing Organization: NASA Langley Research Center"--Report documentation page.
Includes bibliographical references (pages 14-15).
Technical paper.
National Aeronautics and Space Administration 505-31-73-01 L-13868
Other form: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
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
GPO item no.:0830-H-15 (online)
Govt.docs classification:NAS 1.60:1767

MARC

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500 |a Title from title screen (viewed on Aug. 19, 2016). 
500 |a "December 1980." 
500 |a "Performing Organization: NASA Langley Research Center"--Report documentation page. 
504 |a Includes bibliographical references (pages 14-15). 
513 |a Technical paper. 
536 |a National Aeronautics and Space Administration  |d 505-31-73-01  |d L-13868 
650 7 |a Aerodynamic characteristics.  |2 nasat 
650 7 |a Aerodynamic configurations.  |2 nasat 
650 7 |a Angle of attack.  |2 nasat 
650 7 |a Hypersonic aircraft.  |2 nasat 
650 7 |a Supersonic aircraft.  |2 nasat 
650 7 |a Aerodynamics, Supersonic.  |2 fast  |0 http://id.worldcat.org/fast/fst00798221 
650 7 |a Hypersonic planes.  |2 fast  |0 http://id.worldcat.org/fast/fst00965814 
650 7 |a Mach number.  |2 fast  |0 http://id.worldcat.org/fast/fst01004756 
650 7 |a Supersonic wind tunnels.  |2 fast  |0 http://id.worldcat.org/fast/fst01139019 
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