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摘要:
Ring-groove cylindrical shell structures have been applied extensively in some separate devices for aerospace vehicles. In this paper, some research on the optimization and parametric analysis of a ring-groove cylindrical shell structure were given out under lateral explosion impulsion and axial pressure. The large finite element software and a majorized function of MATLAB are selected as analysis platform in there.
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来源 :
Acta Mechanica Solida Sinica
ISSN: 0254-7805
年份: 2007
期: 4
卷: 28
页码: 420-424
2 . 2 0 0
JCR@2022
ESI学科: ENGINEERING;
JCR分区:4
归属院系: