Numerical study of attack angle characteristics for integrated hypersonic vehicle
作者： Wei Huang , Zhen-guo Wang
DOI: 10.1007/S10483-009-0612-Y
关键词: Angle of attack 、 Ignition system 、 Aerospace engineering 、 Longitudinal static stability 、 Component (UML) 、 Head (vessel) 、 Partial differential equation 、 Inlet 、 Airframe 、 Computer science
摘要: The two-dimensional coupled implicit Navier-Stokes equations and standard k-ɛ viscous models are used to simulate the angle of attack characteristics an integrated hypersonic vehicle with a hark head configuration under three kinds working conditions: inlet cut-off, engine through-flow, ignition. Influence each component on aero-propulsive performance is discussed. It concluded that longitudinal static stability good, there enough lift-to-drag ratio satisfy flying requirement vehicle. At same time, it important change configurations upper surface airframe improve
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