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- Algorithm
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- 381kb
- Update:
- 2012-11-26
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Description: 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.
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- [3dc] - Finite volume method in rectangular coor
File list (Check if you may need any files):
mesh
....\Debug
....\mesh.mak
....\mesh.mdp
....\STAGE.GIN
....\STAGESMESH.for
....\新建 Microsoft Word 文档.doc
....\程序介绍说明.pdf