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Some effects of Mach number and geometry on sonic boomMach number and geometry effects on level of sonic boom overpressure and applicability of Whitham theory to calculation of sonic boom
Document ID
19670028998
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Hicks, R. H. (NASA Ames Research Center Moffett Field, CA, United States)
Hunton, L. W. (NASA Ames Research Center Moffett Field, CA, United States)
Mendoza, J. P. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 2, 2013
Publication Date
October 1, 1967
Subject Category
Aerodynamics
Report/Patent Number
NASA-TN-D-4214
Accession Number
67N38327
Funding Number(s)
CONTRACT_GRANT: 720-01-00-02-00-21
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
MACH NUMBER
WIND TUNNEL MODEL
GEOMETRIC FACTOR
SONIC BOOM
HYPERSONIC AIRCRAFT

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