NDLI: Improvement of maneuverability at high subsonic speeds

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Improvement of maneuverability at high subsonic speeds

Content Provider	NASA Technical Reports Server (NTRS)
Author	Staudacher, W.
Organization	The National Aeronautics and Space Administration (NASA)
Copyright Year	1974
Abstract	Results of a series of experimental studies regarding the improvement of the maneuverability of fighter aircraft. The applicability of slotted and unslotted leading edge and trailing edge flaps was tested up to the transonic region on a wind tunnel model as a geometrically variable configuration variant. As a geometrically fixed configuration variant, strakes, or high sweepback leading edge modifications, were attached to the basic delta wing at the wing root and were tested in the entire Mach number range of a fighter aircraft. Through a combination of the maneuver aids improvements of more than 100% over the basic wing could be achieved in certain flight ranges. The efficiency of the strake in the range of high angles of attack considerably exceeds that of the flap system.
File Size	505574
File Format	PDF
Alternate Webpage(s)	http://www.archive.org/details/nasa_techdoc_19740009644
Archival Resource Key	ark:/13960/t6931jz4r
Language	English
Publisher Date	1974-03-01
Access Restriction	Open
Subject Keyword	Radio Waves Venus Atmosphere Wave Propagation Absorption Spectra Atmospheric Refraction Atmospheric Turbulence Electromagnetic Wave Transmission Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science
Content Type	Text

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