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Low-speed static wind-tunnel investigation of a half-span fuselage and variable sweep pressure wing modelLow speed static wind tunnel tests of half-span fuselage and variable sweep pressure wing model
Document ID
19710024300
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Lamar, J. E. (NASA Langley Research Center Hampton, VA, United States)
Mc Kinney, L. W. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
August 1, 1971
Subject Category
Aerodynamics
Report/Patent Number
L-7548
NASA-TN-D-6215
Accession Number
71N33776
Funding Number(s)
CONTRACT_GRANT: 136-13-01-04
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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