Structure parameters optimization on composite flexible pad for aircraft skin stretch forming with reconfigurable tool

被引：0
|
作者：
Wang, Hua [1 ]
Zhou, Xianbin [1 ]
机构：
[1] Department of Aircraft Manufacturing Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100083, China
来源：
Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica | 2007年 / 28卷 / 06期
关键词：
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页码：1482 / 1486
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