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Nonseparating High-Area-Ratio Supersonic NozzlesProcedure determines supersonic-nozzle contours that allow higher nozzle-exit wall pressures, reducing chamber pressure without causing wall-flow separation as encountered in optimum large-area-ratio nozzle designs. Procedure applies to chemical-laser nozzles, jet-engine and gas turbines, wind tunnels and rocket nozzles.
Document ID
19830000657
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Wagner, W. R. (Rockwell International Corp.)
Kassner, R. R. (Rockwell International Corp.)
Date Acquired
August 11, 2013
Publication Date
November 1, 1984
Publication Information
Publication: NASA Tech Briefs
Volume: 8
Issue: 2
ISSN: 0145-319X
Subject Category
Mechanics
Report/Patent Number
MFS-19758
Accession Number
83B10657
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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