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CHARACTERISTICS OF AIRCRAFT WITH LIFTING-FAN PROPULSION SYSTEMS FOR V/STOLWind-tunnel tests on lifting-fan propulsion system for v/stol aircraft - fan-in-fuselage and fan-in-wing configurations are considered
Document ID
19630015522
Acquisition Source
Legacy CDMS
Document Type
Preprint (Draft being sent to journal)
Authors
Goldsmith, R. H.
Hickey, D. H.
Date Acquired
August 1, 2013
Publication Date
January 23, 1963
Subject Category
Biosciences
Report/Patent Number
IAS PAPER 63-27
Report Number: IAS PAPER 63-27
Accession Number
63A11581
Distribution Limits
Public
Copyright
Other
Keywords
VTOL AIRCRAFT
STOL AIRCRAFT
FANLIFT DEVICE

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