Wind-tunnel Investigation of Highly Maneuverable Supersonic V/STOL Fighter PDF Download
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Category :
Languages : en
Pages : 28
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Author:
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Category :
Languages : en
Pages : 28
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Author: David E. Hahne
Publisher:
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Category : Stability of airplanes
Languages : en
Pages : 68
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Category :
Languages : en
Pages : 42
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Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781722350284
Category :
Languages : en
Pages : 46
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Book Description
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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Category : Short take-off and landing aircraft
Languages : en
Pages : 484
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Author:
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Category :
Languages : en
Pages : 78
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Author: Paul L. Coe
Publisher:
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Category : Short take-off and landing aircraft
Languages : en
Pages : 48
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Author:
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Category :
Languages : en
Pages : 24
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Author:
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Category :
Languages : en
Pages : 52
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Author: William A. Newsom
Publisher:
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Category : Aerodynamics
Languages : en
Pages : 88
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