LARGE DEFLECTION AND POST-BUCKLING BEHAVIOR OF SOME LAMINATED PLATES

被引：43

作者：

TURVEY, GJ ^{[1
]}

WITTRICK, WH ^{[1
]}

机构：

[1] UNIV BIRMINGHAM, DEPT CIVIL ENGN, BIRMINGHAM, ENGLAND

来源：

AERONAUTICAL QUARTERLY | 1973年 / 24卷 / MAY期

关键词：

D O I：

10.1017/S0001925900006466

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

页码：77 / 86

页数：10

共 29 条

[21]

THIELMANN W, 1950, NACATM1263

[22]

TURVEY G, 1971, THESIS U BIRMINGHAM

[23] SHEAR BUCKLING OF UNSYMMETRICAL CROSS-PLY PLATES [J].

WHITNEY, JM .

[24] EFFECT OF BOUNDARY CONDITIONS ON RESPONSE OF LAMINATED COMPOSITES [J].

WHITNEY, JM .

WHITNEY, JM ;

LEISSA, AW .

WHITNEY, JM .

[27] ANALYSIS OF HETEROGENEOUS ANISOTROPIC PLATES [J].

WHITNEY, JM ;

LEISSA, AW .

JOURNAL OF APPLIED MECHANICS, 1969, 36 (02) :261-&

[28]

WITTRICK WH, 1972, CONTRIBUTIONS THEORY

[29]

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