Comparison between test and analysis of a tank bulkhead loaded in the plastic range
被引:25
作者:
Becker, W
论文数: 0引用数: 0
h-index: 0
机构:
DAIMLER BENZ AG,AEROSP,ABT RST45,D-88039 FRIEDRICHSHAFEN,GERMANYDAIMLER BENZ AG,AEROSP,ABT RST45,D-88039 FRIEDRICHSHAFEN,GERMANY
Becker, W
[1
]
Wacker, T
论文数: 0引用数: 0
h-index: 0
机构:
DAIMLER BENZ AG,AEROSP,ABT RST45,D-88039 FRIEDRICHSHAFEN,GERMANYDAIMLER BENZ AG,AEROSP,ABT RST45,D-88039 FRIEDRICHSHAFEN,GERMANY
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.