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CHARACTERISTICS OF LIFTING-FAN V/STOL AIRCRAFTWind-tunnel tests of full scale practical configuration of lifting fan v/stol aircraft show transition pitching moments comparable to conventional aircraft, and that lift increases with greater forward speed
Document ID
19630027574
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Goldsmith, R. H.
Hickey, D. H.
Date Acquired
August 1, 2013
Publication Date
October 1, 1963
Subject Category
Biosciences
Accession Number
63A23633
Distribution Limits
Public
Copyright
Other
Keywords
LIFT FAN
AERODYNAMIC LIFT
VTOL AIRCRAFT
STOL AIRCRAFT
PROPULSION CONFIGURATION
WIND TUNNEL STABILITY TEST

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