S1流场计算技术的改进和完善
Improvement of Blade-To-Blade Flow Field Calculation
摘要
采用有黏-无黏相互迭代的研究方法,对已有的S1流场计算程序进行了改进与完善。就数值计算结果与试验结果的对比而言,改进后的S1流场计算程序在精度上基本可以满足工程要求。
A viscid -inviscid iteration method is adopted to improve the present computational program of blade -to - blade flow field. Comparison of the computation and test resuhs shows that the modified blade - to - blade computational program basically meets the engineering precision requirements.
出处
《航空发动机》
2005年第3期50-54,共5页
Aeroengine
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