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Experimental study of wind-tunnel wall effects and wall corrections for a general-research v/stol tilt-wing model with flapWind tunnel wall effects and wall corrections for vertical short takeoff and landing tilt-wing model with flap
Document ID
19650019033
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Grunwald, K. J. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
July 1, 1965
Subject Category
Aerodynamics
Report/Patent Number
NASA-TN-D-2887
Report Number: NASA-TN-D-2887
Accession Number
65N28634
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
WIND TUNNEL WALL
VTOL
TILT-WING AIRCRAFT

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