Numerical study of attack angle characteristics for integrated hypersonic vehicle

Abstract：The two-dimensional coupled implicit Navier-Stokes equations and standard k-ε viscous models are used to simulate the angle of Stack characteristics of an integrated hypersonic vehicle with a hark head configuration under three kinds of working conditions:inlet cut-off,engine through-flow,and engine ignition.Influence of each component on aero-propulsive performance of the vehicle is discussed.It is concluded that the longitudinal static stability of the vehicle is good,and there is enough lift-to-drag ratio to satisfy the flying requirement of the vehicle.At the same time,it is important to change configurations of engine and upper surface of airframe to improve aero-propulsive performance of the vehicle. 作者： Author： Wei HUANG  Zhen-guo WANG 作者單位： Institute of Aerospace and Material Engineering,National University of Defense Technology,Changsha 410073,P.R.China 期 刊： 應用數學和力學（英文版）   EISCI Journal： APPLIED MATHEMATICS AND MECHANICS 年，卷(期)： 2009, 30(6) 分類號： V211 Keywords： integrated hypersonic vehicle    properties of stack angle    component analysis    computer simulation    hark head configuration    aero-propulsive performance    機標分類號： V21 TK1 機標關鍵詞： hypersonic vehicle    integrated    performance    static stability    Navier-Stokes    improve    upper    three    time 基金項目： the Excellent Graduate Student Innovative Project of National University of Defense Technology，Hunan Provincial Innovation Foundation for Postgraduate Numerical study of attack angle characteristics for integrated hypersonic vehicle[期刊論文]  應用數學和力學（英文版） --2009, 30(6)The two-dimensional coupled implicit Navier-Stokes equations and standard k-ε viscous models are used to simulate the angle of Stack characteristics of an integrated hypersonic vehicle with a hark head...

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