ASYMMETRIC POSTBUCKLING OF SYMMETRICALLY LAMINATED CROSS PLY, SHORT CYLINDRICAL PANELS UNDER COMPRESSION

被引：26

作者：

HUI, D

机构：

[1] Ohio State Univ, Boyd Lab, Columbus,, OH, USA, Ohio State Univ, Boyd Lab, Columbus, OH, USA

来源：

COMPOSITE STRUCTURES | 1985年 / 3卷 / 01期

关键词：

AEROSPACE AND OCEAN ENGINEERING - CLOSED CIRCULAR CYLINDRICAL SHELLS - IMPERFECTION SENSITIVITY - LIGHTWEIGHT COMPOSITE MATERIALS;

D O I：

10.1016/0263-8223(85)90029-7

中图分类号：

O3 [力学];

学科分类号：

08 ; 0801 ;

摘要：

引用

页码：81 / 95

页数：15

共 28 条

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[2] A NUMERICAL AND EXPERIMENTAL INVESTIGATION OF THE BUCKLING BEHAVIOR OF COMPOSITE PANELS [J].

BAULD, NR ;

KHOT, NS .

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[3]

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[5] EXPERIMENTAL INVESTIGATION OF THE INSTABILITY OF COMPOSITE CYLINDRICAL PANELS [J].

BECKER, ML ;

PALAZOTTO, AN ;

KHOT, NS .

EXPERIMENTAL MECHANICS, 1982, 22 (10) :372-376

[6]

BOOTON M, 1976, UTIAS203 U TOR I AER

[7]

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[8]

CARD MF, 1969, THESIS VIRGINIA POLY

[9] SHEAR BUCKLING OF ANTI-SYMMETRIC CROSS PLY RECTANGULAR-PLATES [J].

HUI, D .

FIBRE SCIENCE & TECHNOLOGY, 1984, 21 (04) :327-340

[10] EFFECT OF STRINGER TORSIONAL RIGIDITY ON BUCKLING OF INTEGRALLY STIFFENED ANGLE PLY PLATES [J].

HUI, D ;

HANSEN, JS .

FIBRE SCIENCE & TECHNOLOGY, 1982, 16 (01) :39-43

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