Identification technique of constitutive model parameters for crashworthiness modelling

被引:37
作者
Langrand, B
Geoffroy, P
Petitniot, JL
Fabis, J
Markiewicz, E
Drazetic, P
机构
[1] ONERA Lille, Solid & Damage Mech Dept, Structural Resistance & Design Sect 5, F-59000 Lille, France
[2] Univ Valenciennes, Ind & Human Automat Control & Mech Engn Lab, Mech Engn Res Grp, URA CNRS D1775, F-59304 Valenciennes, France
来源
AEROSPACE SCIENCE AND TECHNOLOGY | 1999年 / 3卷 / 04期
关键词
dynamic; compression; material laws; identification; steel;
D O I
10.1016/S1270-9638(99)80044-3
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
This paper deals with a parametric identification technique, based on the conjugate gradient methods. As part of this research, compression tests are performed on a XC48 steel (AFNOR norm 1048AISI), which is strain rate sensitive. Two kinds of specimens, tubular and cylindrical "dumbbell", are tested at different strain rates, from 10(-3) to 130 s(-1) and for impact velocities ranging from 5 mm/min to 6 m/s. The parameters of the Johnson-Cook constitutive model are evaluated directly from the XC48 steel compression stress-strain diagrams expressed in terms of true stress and strain measurements. These parameters are next used as input data for a FE crash simulation of the tubular specimen. Comparison with experimental results prove the validity of the identified parameters. (C) Elsevier, Paris.
引用
收藏
页码:215 / 227
页数:13
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