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Chinese Academy of Sciences Institutional Repositories Grid
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浏览/检索结果: 共14条,第1-10条 帮助

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Reverse jet parameters study on aerodynamic thermal uncertainty of a blunt body 期刊论文  OAI收割
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 107, 页码: 106260
作者:  
Zhang W;  Wang S;  Wang Q;  Ju SJ(鞠胜军);  Yan C
  |  收藏  |  浏览/下载:33/0  |  提交时间:2021/02/09
Dynamic rupture of metal sheet subjected to laser irradiation and tangential subsonic airflow 期刊论文  OAI收割
Theoretical & Applied Mechanics Letters, 2018, 卷号: 8, 期号: 4, 页码: 272-276
作者:  
Xing XD;  Ma T(马特);  Wang RX(王睿星);  Chao CY;  Song HW(宋宏伟)
  |  收藏  |  浏览/下载:44/0  |  提交时间:2018/12/25
Numerical investigation on the thermal protection mechanism for blunt body with forward-facing cavity 期刊论文  OAI收割
SCIENCE CHINA-TECHNOLOGICAL SCIENCES, 2016, 卷号: 59, 期号: 7, 页码: 1120-1129
作者:  
Li, XD;  Hu ZM(胡宗民);  Jiang ZL(姜宗林)
收藏  |  浏览/下载:16/0  |  提交时间:2016/09/14
Thermal/structural/optical integrated design for optical sensor mounted on unmanned aerial vehicle 会议论文  OAI收割
photoelectronic-technology-committee conference, peoples r china, 2016-11-15
作者:  
Zhang, Gaopeng;  Yang, Hongtao;  Mei, Chao;  Wu, Dengshan;  Shi, Kui
收藏  |  浏览/下载:29/0  |  提交时间:2016/10/18
Thermal/structural/optical integrated design for optical window of a high speed aerial optical camera 会议论文  OAI收割
applied optics and photonics, china: optical design and manufacturing technologies, aopc 2015, beijing, china, 2015-05
作者:  
Gaopeng ZHANG;  Hongtao YANG;  Chao MEI;  Kui SHI;  Dengshan WU
收藏  |  浏览/下载:27/0  |  提交时间:2016/01/04
Preparation of high refractive index La2O3-TiO2 glass by aerodynamic levitation technique and effects of Bi2O3 substitution on its thermal and optical properties 期刊论文  OAI收割
CERAMICS INTERNATIONAL, 2014, 卷号: 40, 期号: 3, 页码: 4985-4988
作者:  
Xiang, Heng;  Guan, Lu;  Peng, Zhijian;  Li, Jianqiang
收藏  |  浏览/下载:30/0  |  提交时间:2014/05/06
Thermal-optical analysis for optical window under high Mach flight condition (EI CONFERENCE) 会议论文  OAI收割
2012 International Conference on Optoelectronics and Microelectronics, ICOM 2012, August 23, 2012 - August 25, 2012, Changchun, China
Zhong C.; Ding Y.; Fu J.
收藏  |  浏览/下载:21/0  |  提交时间:2013/03/25
Thermal Protection Efficiency of Forward-facing Cavity and Opposing Jet Combinational Configuration 期刊论文  OAI收割
JOURNAL OF THERMAL SCIENCE, 2012, 卷号: 21, 期号: 4, 页码: 342,347
Haibo Lu; Weiqiang Liu
收藏  |  浏览/下载:29/0  |  提交时间:2013/01/07
Thermal Protection Efficiency of Forward-facing Cavity and Opposing Jet Combinational Configuration 期刊论文  OAI收割
JOURNAL OF THERMAL SCIENCE, 2012, 卷号: 21, 期号: 4, 页码: 342,347
作者:  
Haibo Lu;  Weiqiang Liu
  |  收藏  |  浏览/下载:20/0  |  提交时间:2013/01/07
Thermal-structure analysis of supersonic dome based on three materials (EI CONFERENCE) 会议论文  OAI收割
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:25/0  |  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.