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Low speed wind tunnel investigation of a semispan STOL jet transport wing with deflected thrust and blowing boundary layer controlWind tunnel investigation of static longitudinal aerodynamic characteristics of semispan swept wing for STOL jet transport with deflected thrust and boundary layer control
Document ID
19710020806
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Henderson, R. L. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
July 1, 1971
Subject Category
Aircraft
Report/Patent Number
NASA-TN-D-6256
L-7543
Report Number: NASA-TN-D-6256
Report Number: L-7543
Accession Number
71N30282
Funding Number(s)
CONTRACT_GRANT: 136-62-02-03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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