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.
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References
Zhu, Youlan, et al., Scientm Sinica (1979), Special Issue (II) , 261–280 (in English).
Zhu, Youlan, et al., Acta Mathematicae Applicatae Sinica (1977), No. 3, 12–27 (in Chinese).
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Zhu, Youlan, Zhong, Xichang, Chen, Bingmu and Zhang, Zuomin, Difference Methods for Initial-Boundary-Value Problems and Flow around Bodies, Science Press, Beijing, 1980 (in Chinese) or Springer-Verlag, Heidelberg and Science Press, Beijing, 1986 (in English).
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© 1988 Springer-Verlag Berlin Heidelberg
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You-lan, Z., Bing-mu, C., Xi-chang, Z., Zuo-min, Z. (1988). Solution of Supersonic Regions of Flow around Combined Bodies. In: Difference Methods for Initial-Boundary-Value Problems and Flow Around Bodies. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-662-06707-9_7
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DOI: https://doi.org/10.1007/978-3-662-06707-9_7
Publisher Name: Springer, Berlin, Heidelberg
Print ISBN: 978-3-662-06709-3
Online ISBN: 978-3-662-06707-9
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