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Large-scale wind-tunnel tests of descent performance of an airplane model with a tilt wing and differential propeller thrustWind tunnel tests of wing stall, performance, and longitudinal stability & control of large model v/stol tilt wing transport aircraft
Document ID
19640021081
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Deckert, W. H. (NASA Ames Research Center Moffett Field, CA, United States)
Dickinson, S. O. (NASA Ames Research Center Moffett Field, CA, United States)
Page, V. R. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 2, 2013
Publication Date
October 1, 1964
Subject Category
Biosciences
Report/Patent Number
NASA-TN-D-1857
Report Number: NASA-TN-D-1857
Accession Number
64N30995
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
LONGITUDINAL STABILITY AND CONTROL
TRANSPORT AIRCRAFT
WIND TUNNEL STABILITY TEST
WING STALL
V/STOL AIRCRAFT

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