Cooling passage design optimization of turbine blades based on response surface methodology

被引：0
|
作者：
Yu, Kuahai [1 ]
Yang, Xi [2 ]
Ni, Jun [1 ]
Yue, Zhufeng [1 ]
机构：
[1] School of Mechanics, Civil Engineering and Architecture, Northwestern Polytechnical University, Xi'an 710072, China
[2] School of Materials Science and Engineering, Northwestern Polytechnical University, Xi'an 710072, China
来源：
Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica | 2009年 / 30卷 / 09期
关键词：
13;
D O I：
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中图分类号：
学科分类号：
摘要：
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页码：1630 / 1634
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