OPTIMAL LAMINATED COMPOSITE SHELLS FOR BUCKLING AND VIBRATION

被引：35

作者：

NSHANIAN, YS ^{[1
]}

PAPPAS, M ^{[1
]}

机构：

[1] NEW JERSEY INST TECHNOL,DEPT MECH ENGN,NEWARK,NJ 07102

来源：

AIAA JOURNAL | 1983年 / 21卷 / 03期

关键词：

D O I：

10.2514/3.8090

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

页码：430 / 437

页数：8

共 15 条

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AIAA JOURNAL, 1981, 19 (04) :517-522

[6] OPTIMUM DESIGN OF LAMINATED PLATES UNDER AXIAL-COMPRESSION [J].

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[7]

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[8]

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[9] OPTIMUM DESIGN OF COMPOSITE STRUCTURES WITH STRESS AND DISPLACEMENT CONSTRAINTS [J].

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AIAA JOURNAL, 1976, 14 (02) :131-132

[10]

NSHANIAN YS, 1981, NJIT NV16 REP

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