Steady 2-D and 3-D Supersonic Flow

  • Wai-How Hui
  • Kun Xu


As shown in Section 7.6, in the case of steady flow, for two of the unified coordinates (λ, ξ, η) to be material coordinates, the mesh velocity must be parallel to the fluid velocity, i.e., (U, V, W) = h(u, v, w).


Computational Fluid Dynamics Mach Number Supersonic Flow Godunov Scheme Mach Number Distribution 
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Copyright information

© Science Press Beijing and Springer-Verlag Berlin Heidelberg 2012

Authors and Affiliations

  • Wai-How Hui
    • 1
  • Kun Xu
    • 1
  1. 1.Mathematics DepartmentHong Kong University of Science and TechnologyChina

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