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Powered-lift aircraft technologyPowered lift aircraft have the ability to vary the magnitude and direction of the force produced by the propulsion system so as to control the overall lift and streamwise force components of the aircraft, with the objective of enabling the aircraft to operate from minimum sized terminal sites. Power lift technology has contributed to the development of the jet lift Harrier and to the forth coming operational V-22 Tilt Rotor and the C-17 military transport. This technology will soon be expanded to include supersonic fighters with short takeoff and vertical landing capability, and will continue to be used for the development of short- and vertical-takeoff and landing transport. An overview of this field of aeronautical technology is provided for several types of powered lift aircraft. It focuses on the description of various powered lift concepts and their operational capability. Aspects of aerodynamics and flight controls pertinent to powered lift are also discussed.
Document ID
19900003273
Acquisition Source
Legacy CDMS
Document Type
Special Publication (SP)
Authors
Deckert, W. H.
(NASA Ames Research Center Moffett Field, CA, United States)
Franklin, J. A.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 8, 2013
Publication Date
January 1, 1989
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NASA-SP-501
NAS 1.21:501
LC-89-39482
Report Number: NASA-SP-501
Report Number: NAS 1.21:501
Report Number: LC-89-39482
Accession Number
90N12589
Funding Number(s)
PROJECT: RTOP 505-43-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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