Postbuckling behaviour of a pressurized stiffened composite panel - Part I: Experimental study

被引：22

作者：

Reinoso, J. ^{[1
]}

Blazquez, A. ^{[1
]}

Paris, F. ^{[1
]}

Canas, J. ^{[1
]}

Melendez, J. C.

机构：

[1] Univ Seville, Sch Engn, Grp Elast & Strength Mat, Seville, Spain

来源：

COMPOSITE STRUCTURES | 2012年 / 94卷 / 05期

关键词：

Composite panels; Postbuckling; Stiffened shells; Uniform pressure;

D O I：

10.1016/j.compstruct.2011.12.014

中图分类号：

O3 [力学];

学科分类号：

08 ; 0801 ;

摘要：

Results of an experimental study of the buckling and postbuckling behaviour until the collapse of a cylindrical stiffened composite panel are presented. The specimen is subjected to a uniform pressure on one of its faces using a combination of gas and liquid inside a hermetic box. The present analysis shows the postbuckling load carrying capacity of elements of this kind without developing failure mechanism. Due to the high sensitivity to geometric imperfections of these structures, a simple procedure to obtain their measurements once the specimen is placed in the experimental device is set out. The data registered in these tests will be used for the subsequent validation of the numerical model in order to develop more accurate solutions. This will produce a significant increment in the fidelity of those predictions, making possible a reduction in the number of tests to be performed in real applications. (C) 2011 Elsevier Ltd. All rights reserved.

引用

页码：1533 / 1543

页数：11

共 19 条

[1] Buckling behavior of composite laminated stiffened panels under combined shear-axial compression [J].

Abramovich, H. ;

Weller, T. ;

Bisagni, C. .

JOURNAL OF AIRCRAFT, 2008, 45 (02) :402-413

[2] EFFECT OF GENERAL IMPERFECTIONS ON BUCKLING OF CYLINDRICAL SHELLS [J].

ARBOCZ, J ;

BABCOCK, CD .

JOURNAL OF APPLIED MECHANICS, 1969, 36 (01) :28-&

[3] Post-buckling and collapse experiments of stiffened composite cylindrical shells subjected to axial loading and torque [J].

Bisagni, C ;

Cordisco, P .

COMPOSITE STRUCTURES, 2006, 73 (02) :138-149

[4] Postbuckling behavior of a pressurized stiffened composite panel - Part II: Numerical analysis. Effect of the geometrical imperfections [J].

Blazquez, A. ;

Reinoso, J. ;

Paris, F. ;

Canas, J. .

COMPOSITE STRUCTURES, 2012, 94 (05) :1544-1554

[5] Analytical and Numerical Models of Postbuckling of Orthotropic Symmetric Plates [J].

Blazquez, Antonio ;

Picon, Rafael .

JOURNAL OF ENGINEERING MECHANICS, 2010, 136 (10) :1299-1308

[6] OPTIMIZATION OF COMPOSITE, STIFFENED, IMPERFECT PANELS UNDER COMBINED LOADS FOR SERVICE IN THE POSTBUCKLING REGIME [J].

BUSHNELL, D .

COMPUTER METHODS IN APPLIED MECHANICS AND ENGINEERING, 1993, 103 (1-2) :43-114

[7] POSTBUCKLING ANALYSIS OF RECTANGULAR ORTHOTROPIC PLATES [J].

CHANDRA, R ;

RAJU, BB .

INTERNATIONAL JOURNAL OF MECHANICAL SCIENCES, 1973, 15 (01) :81-97

[8] Postbuckling behaviour of a blade-stiffened composite panel loaded in uniaxial compression [J].

Falzon, BG ;

Stevens, KA ;

Davies, GO .

COMPOSITES PART A-APPLIED SCIENCE AND MANUFACTURING, 2000, 31 (05) :459-468

[9] Effects of imperfections on the buckling response of compression-loaded composite shells [J].

Hilburger, MW ;

Starnes, JH .

INTERNATIONAL JOURNAL OF NON-LINEAR MECHANICS, 2002, 37 (4-5) :623-643

[10] Postbuckling of composite cylinders under external hydrostatic pressure [J].

Hur, Seong-Hwa ;

Son, Hee-Jin ;

Kweon, Jin-Hwe ;

Choi, Jin-Ho .

COMPOSITE STRUCTURES, 2008, 86 (1-3) :114-124

← 1 2 →