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Dynamic and static wind tunnel tests of a flow direction vaneLow-inertia flow-direction vane static and dynamic wind tunnel tests at subsonic and supersonic speeds for in-flight measurement of bust velocities
Document ID
19710013639
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Richardson, N. R. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
April 1, 1971
Subject Category
Instrumentation And Photography
Report/Patent Number
L-7431
NASA-TN-D-6193
Report Number: L-7431
Report Number: NASA-TN-D-6193
Accession Number
71N23115
Funding Number(s)
CONTRACT_GRANT: 720-04-10-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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