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Effect of model forebody shape on perforated tunnel wall interferenceEffect of model forebody shape on perforated supersonic wind tunnel wall interference
Document ID
19680026661
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-1656
Accession Number
68N36133
Funding Number(s)
CONTRACT_GRANT: 720-03-01-08-22
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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