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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.
- Format:
- Book
- Government document
- Author/Creator:
- Pittman, Jimmy L., author.
- Riebe, Gregory D., author.
- Series:
- NASA technical paper ; 1767.
- NASA technical paper ; 1767
- Language:
- English
- Subjects (All):
- Aerodynamics, Supersonic.
- Hypersonic planes.
- Supersonic wind tunnels.
- Mach number.
- Genre:
- Online resources.
- Physical Description:
- 1 online resource (113 pages) : illustrations
- Place of Publication:
- [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, December 1980.
- Notes:
- Title from title screen (viewed on August 19, 2016).
- "December 1980."
- "Performing Organization: NASA Langley Research Center"--Report documentation page
- Includes bibliographical references (pages 14-15).
- Other Format:
- 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
- OCLC:
- 761078951
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