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Inlet-to-inlet shock interference tests final reportExperimental test program and wind tunnel test data obtained during inlet to inlet shock interference tests
Document ID
19650024233
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Motycka, D. L. (Pratt and Whitney Aircraft East Hartford, CT, United States)
Murphy, J. B. (Pratt and Whitney Aircraft East Hartford, CT, United States)
Date Acquired
August 2, 2013
Publication Date
September 1, 1965
Subject Category
Aerodynamics
Report/Patent Number
NASA-CR-264
Report Number: NASA-CR-264
Accession Number
65N33834
Funding Number(s)
CONTRACT_GRANT: NAS2-2079
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
SHOCK WAVE
WIND TUNNEL STABILITY TEST
INTERFERENCE
INLET FLOW
TEST PROGRAM

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