Jet effects on cylindrical afterbodies housing sonic and supersonic nozzles which exhaust against a supersonic stream at angles of attack from 90 ̊to 180 ̊/
by Lovick O. Hayman, Jr., amd Russell W. McDearmon.
Description
- Language(s)
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English
- Published
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Washington : National Aeronautics and Space Administration, [1962]
- Note
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Prepared at Langley Research Center.
"March 1962."
Cover title.
- Physical Description
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49 p. :
ill. ;
26 cm.
Viewability
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University of Illinois at Urbana-Champaign
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