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Opto-mechanical integrated simulation technology of trussed front structure for space solar telescope 会议论文
Beijing, China, 2019-07-07
作者:  Xu, Guangzhou;  Ruan, Ping;  Yang, Jianfeng
收藏  |  浏览/下载：6/0  |  提交时间：2020/03/04
Structural design of zoom system based on linear motor 会议论文
Beijing, China, 2019-07-07
作者:  Yang, Xiaofan;  Yang, Hongtao
收藏  |  浏览/下载：71/0  |  提交时间：2020/03/04
Uncertainties in pressurized thermal shock analyses 会议论文
San Antonio, TX, United states, July 14, 2019 - July 19, 2019
作者:  Niffenegger M;  Garrido OC;  Mora DF;  Qian GA(钱桂安);  Mukin R
收藏  |  浏览/下载：14/0  |  提交时间：2020/11/20
Stress intensity factor of interface crack in the cermet cladding material structure under steady mechanical-thermal coupled loads 会议论文
International Conference on Material Science and Engineering, ICMSE 2016, June 24, 2016 - June 26, 2016
作者:  Yang, Junru;  Chi, Yurong;  Wang, Minglan;  Zhu, Ran
收藏  |  浏览/下载：3/0  |  提交时间：2019/12/31
THERMAL SHOCK BUCKLING OF A FUNCTIONALLY GRADED CIRCULAR PLATE 会议论文
作者:  Zhang, Jinghua;  Zhao, Xingxing
收藏  |  浏览/下载：0/0  |  提交时间：2019/11/15
Thermal shock buckling of a functionally graded circular plate 会议论文
Phoenix, AZ, United states, November 11, 2016 - November 17, 2016
作者:  Zhang, Jinghua;  Zhao, Xingxing
收藏  |  浏览/下载：15/0  |  提交时间：2020/11/15
Coupling Analysis for the Thermo-Acoustic-Vibration Response of a Thin-Walled Box 会议论文
10th International Conference on Vibration Engineering and Technology of Machinery, Manchester ENGLAND, SEP 09-11 2014
作者:  Yang Y(杨焱);  Wu CW(吴臣武)
收藏  |  浏览/下载：19/0  |  提交时间：2015/09/29
The steady-state thermo-mechanical analysis of turbine rotor 会议论文
作者:  Zhuo, Ming;  Yang, Li-Hua;  Yu, Lie
收藏  |  浏览/下载：3/0  |  提交时间：2019/12/02
Analytical solutions of deformation for temperature dependent functionally graded conical shells 会议论文
Hong Kong, Hong kong, December 27, 2011 - December 28, 2011
作者:  Zhang, Jinghua;  Li, Guangze;  Li, Yanyan
收藏  |  浏览/下载：3/0  |  提交时间：2020/11/15
Thermal-structure analysis of supersonic dome based on three materials (EI CONFERENCE) 会议论文
2011 International Conference on Electric Information and Control Engineering, ICEICE 2011, April 15, 2011 - April 17, 2011, Wuhan, China
Jiang Z.; Ai X.; Wei Q.; Liu B.; Jia H.
收藏  |  浏览/下载：17/0  |  提交时间：2013/03/25
To a supersonic missile  a seeker could enhance the aerodynamic ability due to decrease the resistance in flying. At the same time  the primary function of a seeker has been considered as the most important equipment for a missile  due to the importance for cueing of targets and tracking for the final approach. However  the dome of a seeker  which is made up of glass  has poor mechanical performance. Especially  in the higher altitude  for a dome  in which the aerothermal and pressure loads could destroy the structure easily  it is necessary to do the thermal-structure coupled analysis due to varied materials. In the paper  to take the spherical dome of a seeker as a example  the analysis has been completed according to the varied materials consist of MgF2  Al2O3 and ZnS. The temperature loads and the pressure loads derived from the results of fluent analysis has been forced on the surface of dome  which simulates the actual Mach 2.5 in flying. According to the results of coupled analysis  the SEQV stress of the dome radium 80mm based on three materials had reached to 31MPa  which shows that the strength is sufficient for Mach 2.5  and offered the warranty to design the attaching to missile for the dome. At the same time  the results required the flexible mounting for the dome due to the displacements results  which the crystal material couldn't accept. 2011 IEEE.  

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