A parametric lightweight turbine disk structure CAD/CAE integration method

被引：0
|
作者：
Luo, Bin [1 ]
Ding, Shui-Ting [1 ]
Li, Guo [1 ]
机构：
[1] National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics, School of Energy and Power Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100191, China
来源：
Hangkong Dongli Xuebao/Journal of Aerospace Power | 2013年 / 28卷 / 09期
关键词：
15;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
引用
收藏
页码：2083 / 2089
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