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Blockage effects of cone-cylinder bodies on perforated wind tunnel wall interferenceCone-cylinder models tested in supersonic wind tunnel to evaluate effect of wall reflected disturbances on model pressure distributions
Document ID
19680026662
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Mitchell, G. A. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
October 1, 1968
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-X-1655
Accession Number
68N36134
Funding Number(s)
CONTRACT_GRANT: 126-15-02-10-22
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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