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The design of variable Mach number asymmetric supersonic nozzles by two procedures employing inclined and curved sonic lines
Document ID
19930083640
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Syvertson, Clarence A
Savin, Raymond C
Date Acquired
August 16, 2013
Publication Date
March 1, 1953
Report/Patent Number
NACA-TN-2922
Report Number: NACA-TN-2922
Accession Number
93R12930
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
NOZZLES
FLOW, COMPRESSIBLE
WIND TUNNELS

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