Multi-stage turbomachinery impeller mesh generation procedures introduce Hou Leyi group unsteady flow developed in this article multistage turbomachinery impeller grid generation procedure for the grid type for H-, and leaves in front of/behind the extension of the regional network set straight Grid number of Id1 and IDN. Main program MESH_BLADE_STAGES, divided into three parts, the original leaf-type and control parameters from the input program INPUT input, solving procedures for GRID (ZERO), the output process for the OUTPUT.

mesh
....\Debug
....\mesh.mak
....\mesh.mdp
....\STAGE.GIN
....\STAGESMESH.for
....\新建 Microsoft Word 文档.doc
....\程序介绍说明.pdf

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