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Shock Waves pp 161-166 | Cite as

Integration property of a wedge-elliptic cone waverider with scramjet engine

  • H. Liu
  • F. M. Wang
  • L. W. Li
  • Y. B. Geng
Conference paper

Abstract

The hypersonic waverider forebody is designed in this paper. For the present waverider, the undersurface is carved out as a stream surface of a hypersonic inviscid flow field around wedge-elliptic cone, and the upper surface is assumed to be a freestream surface. A finite-volume code is used to generate the three-dimensional flow field. The leading edge is determined by satisfying the condition that the lip is situated at the intersection line of shocks.

Keywords

Shock Wave Flow Field AIAA Paper Wedge Angle Pressure Contour 
These keywords were added by machine and not by the authors. This process is experimental and the keywords may be updated as the learning algorithm improves.

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Copyright information

© Tsinghua University Press and Springer-Verlag Berlin Heidelberg 2005

Authors and Affiliations

  • H. Liu
    • 1
  • F. M. Wang
    • 1
  • L. W. Li
    • 1
  • Y. B. Geng
    • 1
  1. 1.Institute of MechanicsChinese academy of SciencesBeijingChina

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