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Experimental study of shock-panel coupling - Preliminary resultsShock-panel coupling effects of supersonic turbulent flow driven by impedance head
Document ID
19680026566
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Cockburn, J. A. (Wyle Labs., Inc. Huntsville, AL, United States)
Date Acquired
August 4, 2013
Publication Date
March 1, 1968
Subject Category
Aerodynamics
Report/Patent Number
TM-68-3
NASA-CR-61986
Report Number: TM-68-3
Report Number: NASA-CR-61986
Accession Number
68N36038
Funding Number(s)
CONTRACT_GRANT: NAS8-21100
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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