三维C-H网格下跨音压气机转子Euler流场数值模拟
NUMERICAL SIMULATION OF 3-D FIELD WITHIN A COMPRESSOR ROTOR WITH C-H GRID
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摘要: 介绍了三维C-H网格的生成和全三维转子流场的数值解。以法国宇航院设计的一个高负荷跨音转子为算例, 并与他们的计算结果作了比较。应用这套数值模拟技术得以计算带进口预旋的某跨音压气机转子流场, 并对进口预旋对其下游的转子流场的影响作了数值模拟, 得出了若干有意义的结论。Abstract: A 3-D C-H grid generation technique and 3-D Euler governing equation are described briefly.The highly loaded transonic compressor rotor designed by ONERA is taken as a numerical example.ONERA′S numerical results and ours with H grid and C-H grid are compared respectively in respect of the pressure distributions along profiles at hub and tip of the rotor.The numerical technique presented is applied to evaluating the influence of inlet pre swirl on its downstream flow field in the rotor,in result a new numerical approach is obtained for design optimization of pre swirl distribution at compressor design stage.As numerical examples,two kinds of pre swirl distributions are examined to show its influence on Mw1 、β1 and α2 etc. distributions along radius.
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