Comparison between test and analysis of a tank bulkhead loaded in the plastic range

被引:25
作者
Becker, W [1 ]
Wacker, T [1 ]
机构
[1] DAIMLER BENZ AG,AEROSP,ABT RST45,D-88039 FRIEDRICHSHAFEN,GERMANY
来源
AEROSPACE SCIENCE AND TECHNOLOGY | 1997年 / 1卷 / 01期
关键词
tank structure; finite element analysis; plastic yielding; nonlinear; ultimate failure analysis;
D O I
10.1016/S1270-9638(97)90025-0
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
For qualification and verification, the common bulkhead of the Ariane 5 tank structure has been submitted to detailed finite element analyses by means of the finite element code ABAQUS. In doing so the doubly curved variable-thickness geometry of the bulkhead segments has been discretized by a sufficiently fine shell element meshing and the finite element analyses have been extended far into the geometrically and physically nonlinear regime. A proof pressure load case has been evaluated and an ultimate failure analysis has been performed. The calculated results correspond well with test findings and qualify ABAQUS as a very good dimensioning tool for highly stressed thin walled structures.
引用
收藏
页码:77 / 81
页数:5
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[1]  
*HIBB KARLSS SOR I, ABAQUS VERS 5 3