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Proposed Short-Throat Supersonic NozzlesNumerical procedure analyzes mach numbers along wall and in flow field, wall pressures, gas temperatures, and nozzle-throat discharge coefficients. Nozzles used in turbines, jet engines, magnetohydrodynamic systems, laser systems and other supersonic-flow devices.
Document ID
19830000067
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Wagner, W. R. (Rockwell International Corp.)
Ratekin, G. H. (Rockwell International Corp.)
Date Acquired
August 11, 2013
Publication Date
August 1, 1983
Publication Information
Publication: NASA Tech Briefs
Volume: 7
Issue: 3
ISSN: 0145-319X
Subject Category
Mechanics
Report/Patent Number
MFS-19759
Accession Number
83B10067
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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