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Wall effect and scale effect in v/stol model testingWind-tunnel wall effect on tilt-wing and fan-in- wing aircraft models
Document ID
19640007100
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Grunwald, K. J. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 2, 2013
Publication Date
March 10, 1964
Subject Category
Biosciences
Accession Number
64N17014
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
FAN-IN-WING AIRCRAFT
TILT-WING AIRCRAFT
WIND TUNNEL MODEL

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