Solution of Supersonic Regions of Flow around Combined Bodies

Zhu You-lan, Chen Bing-mu, Zhong Xi-chang and Zhang Zuo-min
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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

Chapter Chapter 7 in Difference Methods for Initial-Boundary-Value Problems and Flow Around Bodies, 1988, pp 423-572 from Springer

Abstract: 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.

Keywords: Flow Field; Main Shock; Free Stream; Expansion Wave; Contact Discontinuity (search for similar items in EconPapers)
Date: 1988
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DOI: 10.1007/978-3-662-06707-9_7

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