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Status of v/stol research and development in the united statesIt is the purpose of this paper to review the status of V/-STOL research and development in the United States with particular emphasis on significant research results obtained since the last Anglo-American Conference in 1961. Research information will be presented dealing with the helicopter, with propeller, ducted-fan, and jet V/STOL aircraft, and with the general area of V/STOL handling-qualities requirements.
Document ID
19640018315
Acquisition Source
Langley Research Center
Document Type
Other - NASA Reference Publication (RP)
Authors
John P Campbell (Langley Research Center Hampton, Virginia, United States)
Date Acquired
August 2, 2013
Publication Date
May 1, 1964
Publication Information
Publication: Journal of Aircraft
Publisher: American Institute of Aeronautics and Astronautics
Volume: 1
Issue: 3
Issue Publication Date: May 1, 1964
ISSN: 0021-8669
e-ISSN: 1533-3868
DOI: 10.2514/3.43576
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NASA-RP-286
Report Number: NASA-RP-286
Meeting Information
Meeting: 9th Anglo-American Conference
Location: Cambridge, MA
Country: US
Start Date: October 16, 1963
End Date: October 18, 1963
Sponsors: Royal Aeronautical Society, Canadian Aeronautics and Space Institute
Accession Number
64N28229
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
V/STOL aircraft
Turbojet aircraft
Ducted fan engine
Helicopter
Aeroplane
Rotor systems
Angle of descent
Handling qualities
Turbofan
Wind tunnels
Tip speed ratio
NASA Langley Research Center
Fuselage configurations
Lift coefficient
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