Method for obtaining aerodynamic data on hypersonic configurations with scramjet exhaust flow simulation /
William R. Hartill.

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Main Author: Hartill, William R.
Related Names: United States. National Aeronautics and Space Administration.
Language(s): English
Published: Washington : National Aeronautics and Space Administration ; 1977.
Subjects: Hypersonic wind tunnels > Hypersonic wind tunnels / Equipment and supplies.
Jets > Jets / Fluid dynamics.
Airplanes > Airplanes / Ramjet engines > Airplanes / Ramjet engines / Combustion.
Airplanes > Airplanes / Scramjet engines.
Aerodynamics, Hypersonic.
Hypersonic planes > Hypersonic planes / Models > Hypersonic planes / Models / Testing.
Note: Issued June 1977.
Prepared by Rockwell International Corporation, Los Angeles Aircraft Division, under contract no. NAS1-14320.
Physical Description: iv, 74 p. : ill. ; 27 cm.
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