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A rapid graphical method for computing the pressure distribution at supersonic speeds on a slender arbitrary body of revolution
Document ID
19930082441
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Thompson, Jim Rogers
Date Acquired
August 16, 2013
Publication Date
January 1, 1949
Report/Patent Number
NACA-TN-1768
Report Number: NACA-TN-1768
Accession Number
93R11731
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
THEORIES - FLOW SUPERSONIC
FLOW - BODIES SUPERSONIC
PRESSURE DISTRIBUTION - BODIES

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