Wind-tunnel Investigation of Highly Maneuverable Supersonic V/STOL Fighter
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Page : 28 pages
File Size : 13,90 MB
Release : 1979
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Page : 28 pages
File Size : 13,90 MB
Release : 1979
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Author : David E. Hahne
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Page : 68 pages
File Size : 39,17 MB
Release : 1993
Category : Stability of airplanes
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Page : 42 pages
File Size : 21,13 MB
Release : 1984
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Page : 484 pages
File Size : 15,32 MB
Release : 1979
Category : Short take-off and landing aircraft
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Author : National Aeronautics and Space Administration (NASA)
Publisher : Createspace Independent Publishing Platform
Page : 46 pages
File Size : 36,57 MB
Release : 2018-07-05
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ISBN : 9781722350284
A wind-tunnel investigation was conducted to examine the low-speed static stability and control characteristics of a 0.10 scale model of a STOL supersonic cruise fighter concept. The concept, referred to as a twin boom fighter, was designed as a STOL aircraft capable of efficient long range supersonic cruise. The configuration name is derived from the long twin booms extending aft of the engine to the twin vertical tails which support a high center horizontal tail. The propulsion system features a two dimensional thrust vectoring exhaust nozzle which is located so that the nozzle hinge line is near the aircraft center of gravity. This arrangement is intended to allow large thrust vector angles to be used to obtain significant values of powered lift, while minimizing pitching moment trim changes. Low speed stability and control information was obtained over an angle of attack range including the stall. A study of jet induced power effects was included. Coe, Paul L., Jr. and Riley, Donald R. Langley Research Center RTOP 505-61-71-07...
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Page : 78 pages
File Size : 28,9 MB
Release : 1984
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Author : Paul L. Coe
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Page : 48 pages
File Size : 45,26 MB
Release : 1988
Category : Short take-off and landing aircraft
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Page : 24 pages
File Size : 14,7 MB
Release : 1988
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Page : 52 pages
File Size : 20,27 MB
Release : 1962
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Author : William A. Newsom
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Page : 88 pages
File Size : 31,87 MB
Release : 1959
Category : Aerodynamics
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