NONLINEAR RESPONSE OF ASYMMETRICALLY LAMINATED PLATES IN CYLINDRICAL BENDING

被引：19

作者：

CARRERA, E

机构：

[1] DIAS-Politecnico di Torino, Torino

来源：

AIAA JOURNAL | 1993年 / 31卷 / 07期

关键词：

D O I：

10.2514/3.11780

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

[No abstract available]

引用

页码：1353 / 1357

页数：5

共 12 条

[1]

AMBARTSUMYAN SA, 1964, NASA TTF118

[2] NONLINEAR-ANALYSIS OF COMPOSITE LAMINATES USING A GENERALIZED LAMINATED PLATE-THEORY [J].

BARBERO, EJ ;

REDDY, JN .

AIAA JOURNAL, 1990, 28 (11) :1987-1994

[3] THE EFFECTS OF SHEAR DEFORMATION AND CURVATURE ON BUCKLING AND VIBRATIONS OF CROSS-PLY LAMINATED COMPOSITE SHELLS [J].

CARRERA, E .

JOURNAL OF SOUND AND VIBRATION, 1991, 150 (03) :405-433

[4]

CARRERA E, 1991, THESIS TORINO

[5] CYLINDRICAL BENDING OF UNSYMMETRIC COMPOSITE LAMINATES [J].

CHEN, HP ;

SHU, JC .

AIAA JOURNAL, 1992, 30 (05) :1438-1440

[6]

Chia C.Y., 1980, NONLINEAR ANAL PLATE

[7] STATIC BUCKLING OF MODERATELY THICK, ANISOTROPIC, LAMINATED AND SANDWICH CYLINDRICAL-SHELL PANELS [J].

DISCIUVA, M ;

CARRERA, E .

AIAA JOURNAL, 1990, 28 (10) :1782-1793

[8] CONDITIONS FOR LAMINATED PLATES TO REMAIN FLAT UNDER INPLANE LOADING [J].

LEISSA, AW .

COMPOSITE STRUCTURES, 1986, 6 (04) :261-270

[9]

PALAZOTTO AN, 1992, AIAA ED SERIES

[10]

STAVSKY Y, 1961, J APPLIED MECHANICS, V28, P402

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