Conceptual Design and Numerical Simulations of Hypersonic Waverider Vehicle

【Author】

C.H.Lee;

【Abstract】

<正>A modularized airframe/propulsion integrated model is established by oblique shock wave theory,engineering method and method of characteristics(MOC).Based on this method,a new design methodology for hypersonic waverider vehicle which integrated scramjets with waverider airframe derived from cone-wedge flow field is presented.Integrated aero-propulsion performance of the waverider vehicle under on-design and off-design conditions is predicted using Euler equations discretized by Harten-Yee non-MUSCL TVD scheme and the combustor flow field is approximated by a quasi-1D cycle analysis, skin friction of vehicle is calculated by reference temperature method.

【Keywords】

Conceptual Design and Numerical Simulations of Hypersonic Waverider Vehicle;

References

To explore the background and basis of the node document

Springer Journals Database

Total: 4 articles

  • [1] ZHAO Guilin HU Liang WEN Jie PENG Hui ZHANG Mianchun Institute of Mechanics, Chinese Academy of Sciences, Beijing 100080, China Dept. of Jet Propulsion, Beijing Univ. of Aeronautics and Astronautics, Beijing 100083, China, AN OVERVIEW OF THE RESEARCH ON WAVERIDERS AND WAVERIDER-DERIVED HYPERSONIC VEHICLES, Advances In Mechanics,
  • [2] Bo Zheng;;Chun-Hian Lee, The effects of limiters on high resolution computations of hypersonic flows over bodies with complex shapes, Communications in Nonlinear Science and Numerical Simulation,
  • [3] Mary Kae Lockwood O‘Neill;Lewis Mark J, Design tradeoffson scramjet engine integrated hypersonic waverider vehicles, Journal of Aircraft, Journal of Aircraft (Journal of Aircraft)
  • [4] Zheng B, Lee C H, The effects of limiters on high resolution computations of hypersonic flows over bodies with complex shapes, Comm Nonlin Sci Numer Simul,

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