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Solution of Supersonic Regions of Flow around Combined Bodies

In: Difference Methods for Initial-Boundary-Value Problems and Flow Around Bodies

Author

Listed:
  • Zhu You-lan

    (Chinese Academy of Sciences, Computing Center)

  • Chen Bing-mu

    (Chinese Academy of Sciences, Computing Center)

  • Zhong Xi-chang

    (Chinese Academy of Sciences, Computing Center)

  • Zhang Zuo-min

    (Chinese Academy of Sciences, Computing Center)

Abstract

In this chapter, we discuss a numerical method for supersonic regions of three-dimensional flow around combined bodies. The flow under consideration is the steady in viscid, non-heat-conducting flow of a perfect gas or air in chemical equilibrium. If the initial data are given on a space-like surface near the nose of a body, and if the flow in the downstream region of the initial surface is supersonic, then the flow in the supersonic region can be determined by solving an initial-boundary-value problem for hyperbolic systems.

Suggested Citation

  • Zhu You-lan & Chen Bing-mu & Zhong Xi-chang & Zhang Zuo-min, 1988. "Solution of Supersonic Regions of Flow around Combined Bodies," Springer Books, in: Difference Methods for Initial-Boundary-Value Problems and Flow Around Bodies, chapter 0, pages 423-572, Springer.
    • Handle: RePEc:spr:sprchp:978-3-662-06707-9_7
    DOI: 10.1007/978-3-662-06707-9_7
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