NDLI: Powered-lift aircraft technology

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Powered-lift aircraft technology

Content Provider	NASA Technical Reports Server (NTRS)
Author	Deckert, W. H. Franklin, J. A.
Copyright Year	1989
Description	Powered 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.
File Size	14025591
Page Count	36
File Format	PDF
Alternate Webpage(s)	http://archive.org/details/NASA_NTRS_Archive_19900003273
Archival Resource Key	ark:/13960/t3cz8450m
Language	English
Publisher Date	1989-01-01
Access Restriction	Open
Subject Keyword	Aircraft Design, Testing And Performance Vertical Landing C-17 Aircraft Vertical Takeoff Aerodynamics Aerodynamic Coefficients Aircraft Design Short Takeoff Aircraft Aeronautical Engineering Powered Lift Aircraft Lift Vertical Takeoff Aircraft Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science
Content Type	Text
Resource Type	Technical Report

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