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Flow field properties near an arrow wing-body model at Mach numbers of 1.60, 2.36, and 2.96Wind tunnel tests at Mach 1.60, 2.36, and 2.96 to determine flow field properties near arrow wing body model for locating potential engine air inlets
Document ID
19680027766
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Vahl, W. A. (NASA Langley Research Center Hampton, VA, United States)
Weirich, R. L. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
October 1, 1968
Subject Category
Aerodynamics
Report/Patent Number
NASA-TN-D-4809
Accession Number
68N37238
Funding Number(s)
CONTRACT_GRANT: 720-03-00-02-23
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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