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锥柱形膜片后屈曲的材料特性预示研究 被引量:6

EFFECTS OF MATERIAL PROPERTIES ON POST-BUCKLING OF SPHERICAL-CONE DIAPHRAGMS FOR POSITIVE EXPULSION TANKS
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摘要 使用正交表设计数值试验,分析弹性模量、屈服强度、延伸率等材料特性参数对锥柱形膜片结构后屈曲状态的影响,预示材料特性对膜片翻转的影响.正交数值试验在不影响结果科学性的基础上,极大地降低了试验次数.数值试验结果表明:在一定结构情况下,弹性模量与屈服强度对膜片正向翻转影响非常显著,而延伸率的影响与前两个因素比较而言,几乎可以忽略.并且,结构顶点位移随材料的弹性模量增大而增大;随材料的屈服强度减小而增大.因此,在结构固定的情况下,为了提高材料的翻转性能,可以选择弹性模量较大而屈服强度较小的材料,且延伸率为20%左右最好. This paper numerically analyzes the effects of elastic modulus,yield stress and elongation percentage on the post-buckling of spherical-cone diaphragms for positive expulsion tanks based on orthogonal tests.With orthogonal tests,the number of tests is greatly reduced,without affecting the validity of results.Numerical results are as follows:according to the specific diaphragm considered in the paper,its elastic modulus and yield stress have a marked effect on its post-buckling,while the elongation percentage hardly affects the post-bucking of the structure.The top node displacement of diaphragms increases with the increase of the elastic modulus and the decrease of the yield stress.As a result,large elastic modulus,small yield stress and about 20%of elongation will be optimal for diaphragm expulsion.
出处 《力学与实践》 CSCD 北大核心 2012年第2期24-28,共5页 Mechanics in Engineering
基金 国家973计划资助项目(61338)
关键词 锥柱形膜片 材料特性 正交试验 数值分析 后屈曲 spherical-cone diaphragms material properties orthogonal test numerical analysis post-buckling
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  • 1梁辉,孙雨果.推进剂贮箱结构变厚度优化[J].宇航学报,2007,28(5):1349-1352. 被引量:7
  • 2何成旦,李鹤岐,李春旭,应磊,罗岩.隔膜贮箱电子束焊接技术研究[J].真空与低温,2004,10(3):168-171. 被引量:4
  • 3陈志坚,李治,吴建军.推进剂贮箱复合膜研究[J].火箭推进,2005,31(1):21-23. 被引量:1
  • 4周仕明,袁杰红.金属膜片贮箱膜片变形的数值模拟与失效分析[J].上海航天,2005,22(6):13-16. 被引量:26
  • 5布查南G R.有限元分析[M].北京:科学出版社,2002.
  • 6王勖成.有限单元法.北京:清华大学出版社,2005.
  • 7[2]Kammerer H,Hughes J,Gribben E.Analytical & material advances in contoured metal diaphragms for positive expulsion tanks,AIAA 95-2354.
  • 8[1]Marvin M,Kammerer H,Gidley J T.Parametric Evaluation of Contoured Aluminum Diaphragm Positive Expulsion Tanks[C].AIAA/SAE/ASME/ASEE 28th Joint Propulsion Conference and Exhibit July 6-8,1992/Nashville,TN.
  • 9[2]Kammerer H,Hughes J,Gribben E.Analytical & Material Advances in Contoured Metal Diaphragms for Positive Expulsion Tanks[C].31th AIAA/SAE/ASME/ASEE Joint Propulsion Conference and Exhibit July 10-12,1995/San Diego,CA.
  • 10[4]Stanley S,Smeltzer,Lynn M Bowman.Buckling design studies of inverted-oblate bulkheads for a propellant tank[C].43rd AIAA/ASME/ASCE/AHS/ASC Structures Structural Dynamics and Material Con 22-25 April 2002 Denver ColOrado.

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