STATIC RESPONSE OF A CYLINDRICAL COMPOSITE PANEL WITH CUTOUTS USING A GEOMETRICALLY NONLINEAR-THEORY

被引：18

作者：

DENNIS, ST ^{[1
]}

PALAZOTTO, AN ^{[1
]}

机构：

[1] USAF,INST TECHNOL,WRIGHT PATTERSON AFB,OH 45433

来源：

AIAA JOURNAL | 1990年 / 28卷 / 06期

关键词：

D O I：

10.2514/3.25170

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

A geometrically nonlinear static shell theory allowing large displacements and rotations and parabolic transverse shear is developed. The theory is cast into a total Lagrangian finite-element formulation for approximate solutions. The approach is then applied to the problem of an axially compressed quasiisotropic cylindrical shell panel with a cutout up to and beyond collapse. Analytical results compare very well with experimental findings for both global and local panel response. © 1990 American Institute of Aeronautics and Astronautics, Inc., All rights reserved.

引用

页码：1082 / 1088

页数：7

共 29 条

[1]

BAULD NR, 1979, AFFDLTR793038

[2] INSTABILITY OF COMPOSITE PANELS [J].

BECKER, ML ;

PALAZOTTO, AN ;

KHOT, NS .

JOURNAL OF AIRCRAFT, 1981, 18 (09) :739-743

[3]

BUSHNELL D, 1985, FINITE ELEMENTS ANAL, V1

[4] TRANSVERSE-SHEAR DEFORMATION IN ORTHOTROPIC CYLINDRICAL PRESSURE-VESSELS USING A HIGHER-ORDER SHEAR THEORY [J].

DENNIS, ST ;

PALAZOTTO, AN .

AIAA JOURNAL, 1989, 27 (10) :1441-1447

[5]

DENNIS ST, IN PRESS INT J NONLI

[6]

Gallagher R.H., 1975, FINITE ELEM ANAL DES

[7]

HERBERT JS, 1984, 12TH P SE C THEOR AP, P124

[8]

HERMSEN MF, 1986, NONLINEAR ANAL NDE C, V115, P43

[9] EXPERIMENTAL BUCKLING OF CYLINDRICAL COMPOSITE PANELS WITH ECCENTRICALLY LOCATED CIRCULAR DELAMINATIONS [J].

HORBAN, B ;

PALAZOTTO, A .

JOURNAL OF SPACECRAFT AND ROCKETS, 1987, 24 (04) :349-352

[10] COLLAPSE ANALYSIS OF CYLINDRICAL COMPOSITE PANELS WITH CUTOUTS [J].

JANISSE, TC ;

PALAZOTTO, AN .

JOURNAL OF AIRCRAFT, 1984, 21 (09) :731-733

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