PDF下载 分享
[1]朱志华,胡小平,陈香林,等.钛制金属贮箱膜片的有限元分析[J].火箭推进,2007,33(04):32-35.
 Zhu Zhihua,Hu Xiaoping,Chen Xianglin.Finite element analysis of the overturning process of titanium diaphragm for propellant tank[J].Journal of Rocket Propulsion,2007,33(04):32-35.
点击复制

钛制金属贮箱膜片的有限元分析

相似文献/References:

[1]刘晓伟,刘 昊,张蒙正.RBCC火箭对直扩通道抗反压能力的影响研究[J].火箭推进,2015,41(06):7.
 LIU Xiaowei,LIU Hao,ZHANG Mengzheng.Influence of RBCC rocket on resisting backpressure ability of straight-expanded flowpath[J].Journal of Rocket Propulsion,2015,41(04):7.
[2]刘海丽,张立强,李学华,等.低比转速高速泵螺壳形式对性能影响分析[J].火箭推进,2015,41(03):52.
 LIU Hai-li,ZHANG Li-qiang,LI Xue-hua,et al.Influence of volute case type for low-specific-speed pump on pump performance[J].Journal of Rocket Propulsion,2015,41(04):52.
[3]刘红珍,田 原,孙纪国.液氧甲烷单喷嘴燃烧性能数值仿真研究[J].火箭推进,2014,40(01):56.
 LIU Hong-zhen,TIAN Yuan,SUN Ji-guo.Numerical simulation of combustion performance of LOX/methane single nozzle[J].Journal of Rocket Propulsion,2014,40(04):56.
[4]林奇燕,金志磊,王 磊.超音速复速级涡轮的气动设计改进[J].火箭推进,2014,40(01):65.
 LIN Qi-yan,JIN Zhi-lei,WANG Lei.Aerodynamic redesign of supersonic Curtis-stage turbine[J].Journal of Rocket Propulsion,2014,40(04):65.
[5]王朝晖,叶小明.液体火箭发动机氢燃料涡轮三维非定常流场数值研究[J].火箭推进,2014,40(03):38.
 WANG Zhao-hui,YE Xiao-ming.Numerical study of 3-D unsteady flow field in hydrogen fuel turbine of LRE[J].Journal of Rocket Propulsion,2014,40(04):38.
[6]毋 杰,徐 楠,杨大昱,等.半开式离心泵叶顶间隙对泵性能稳定性的影响[J].火箭推进,2014,40(04):29.
 WU Jie,XU Nan,YANG Da-yu,et al.Influence of tip clearance of semi-open centrifugal pump on performance stability[J].Journal of Rocket Propulsion,2014,40(04):29.
[7]张 亮,吴海波,张德禹,等.液体火箭发动机推力室喉部结构热疲劳寿命预估研究[J].火箭推进,2014,40(05):24.
 Study on predicting thermal fatigue life for throat structure of LRE thrust chamber.Study on predicting thermal fatigue life for throat structure of LRE thrust chamber[J].Journal of Rocket Propulsion,2014,40(04):24.
[8]潘 亮,聂 嵩,刘业奎.环槽式过氧化氢/煤油气液喷注器研究[J].火箭推进,2012,38(03):23.
 PAN Liang,NIE Song,LIU Ye-kui.Investigation of circular slot hydrogen peroxide/kerosene injector[J].Journal of Rocket Propulsion,2012,38(04):23.
[9]宋大亮,周立新,陈建华,等.离心式喷嘴全流场数值模拟[J].火箭推进,2011,37(05):36.
 SONG Da-liang,ZHOU Li-xin,CHEN Jian-hua,et al.Numerical simulation of full flowfield of centrifugal nozzle[J].Journal of Rocket Propulsion,2011,37(04):36.
[10]刘洪坤,王维彬.发动机起动燃气返腔仿真与影响分析[J].火箭推进,2011,37(02):30.
 LIU Hong-kun,WANG Wei-bin.Backflow simulation and its influence analysis for gas generator of LRE[J].Journal of Rocket Propulsion,2011,37(04):30.

更新日期/Last Update: 1900-01-01