机译:用于载人气密模块的结构设计的Shakedown分析
Beijing Inst Spacecraft Syst Engn 104 Youyi Rd Beijing 100094 Peoples R China;
Beijing Inst Spacecraft Syst Engn 104 Youyi Rd Beijing 100094 Peoples R China;
Rhein Westfal TH Aachen Inst Mat Applicat Mech Engn Augustinerbach 4 D-52062 Aachen Germany;
Rhein Westfal TH Aachen Inst Mat Applicat Mech Engn Augustinerbach 4 D-52062 Aachen Germany;
Beijing Inst Spacecraft Syst Engn 104 Youyi Rd Beijing 100094 Peoples R China;
Beijing Inst Spacecraft Syst Engn 104 Youyi Rd Beijing 100094 Peoples R China;
Rhein Westfal TH Aachen Inst Mat Applicat Mech Engn Augustinerbach 4 D-52062 Aachen Germany;
Rhein Westfal TH Aachen Inst Mat Applicat Mech Engn Augustinerbach 4 D-52062 Aachen Germany;
Manned airtight module; Shakedown; Direct method (DM); Lightweight design;
机译:用于载人气密模块的结构设计的Shakedown分析
机译:可部署生境模块的结构设计和影响分析
机译:可部署生境模块的结构设计和影响分析
机译:使用可打印相变化合物优化功率模块和基板的热性能,作为预先应用的结构设计
机译:基于金属材料和结构的循环非弹性行为和减振设计:分析与实验
机译:H因子(模块10–15)的中心部分很紧凑并且包含结构上偏差的CCP模块
机译:复合船体模块上压壳结构设计与分析