NUMERICAL CALCULATION TECHNIQUE FOR LARGE ELASTIC-PLASTIC TRANSIENT DEFORMATIONS OF THIN SHELLS

被引:20
作者
LEECH, JW
WITMER, EA
PIAN, THH
机构
[1] Massachusetts Institute of Technology, Cambridge, MA
[2] Massachusetts Institute of Technology, Aeroelastic and Structures Research Laboratory, Cambridge, MA
[3] Massachusetts Institute of Technology, Aeronautics and Astronautics, Cambridge, MA
关键词
D O I
10.2514/3.4994
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Studies of explosive forming of structures must often include the large-deformation transient and permanent-deflection responses of the structure. To aid in studies of this nature, a large-deflection elastic- plastic transient response prediction method has been developed. The accuracy and reliability of this method have been demonstrated by comparisons of theoretical predictions with experimental measurements. The large-deflection large- rotation small-strain equations of motion for a thin shell including elastic, elastic- plastic, strainhardening, and strain-rate material behavior are presented in tensor form. These equations are then cast into numerical form by finite differencing. The step-by-step numerical-integration technique is applied to the case of a cylindrical panel; dynamic-deformation predictions are compared with experimentally observed deformation histories of an explosively loaded cylindrical panel tested at the Picatinny Arsenal. © 1968 American Institute of Aeronautics and Astronautics, Inc., All rights reserved.
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页码:2352 / &
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