Post-buckling and collapse experiments of stiffened composite cylindrical shells subjected to axial loading and torque

被引:57
作者
Bisagni, C [1 ]
Cordisco, P [1 ]
机构
[1] Politecn Milan, Dipartimento Ingn Aerospaziale, I-20156 Milan, Italy
关键词
stiffened shells; composite; failure; post-buckling; compression; torque;
D O I
10.1016/j.compstruct.2005.11.055
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
Experimental data obtained from buckling and post-buckling tests performed until collapse oil three stiffened composite cylindrical shells are described. The shells, different in the skin and in the stiffeners lay-up, were expressly designed for working in the post-buckling field. The outer and inner surfaces are scanned before the tests, in order to determine the initial geometric imperfections and the thickness variations. After that, the shells are tested using a position control mode until collapse, two of them under axial compression and one under torque. The diagrams of axial load versus displacement and of torsion versus rotation are recorded in real time during the tests. To monitor the first buckling load and the evolution of the buckling shape, five laser displacement sensors are employed. The test results show the strength capacity of these structures to work in the post-buckling range. Indeed neither failure mechanisms nor any other hazards are visible in the post-buckling range. On the other hand, the collapse, due to the failure of the stringers, is sudden and destructive. (c) 2005 Elsevier Ltd. All rights reserved.
引用
收藏
页码:138 / 149
页数:12
相关论文
共 17 条
[1]   Future directions and challenges in shell stability analysis [J].
Arbocz, J ;
Starnes, JH .
THIN-WALLED STRUCTURES, 2002, 40 (09) :729-754
[2]   Testing of stiffened composite cylindrical shells in the postbuckling range until failure [J].
Bisagni, C ;
Cordisco, P .
AIAA JOURNAL, 2004, 42 (09) :1806-1817
[3]   An experimental investigation into the buckling and post-buckling of CFRP shells under combined axial and torsion loading [J].
Bisagni, C ;
Cordisco, P .
COMPOSITE STRUCTURES, 2003, 60 (04) :391-402
[4]   Experimental buckling of thin composite cylinders in compression [J].
Bisagni, C .
AIAA JOURNAL, 1999, 37 (02) :276-278
[5]   BUCKLING OF IMPERFECT ANISOTROPIC CIRCULAR-CYLINDERS UNDER COMBINED LOADING [J].
BOOTON, M ;
TENNYSON, RC .
AIAA JOURNAL, 1979, 17 (03) :278-287
[6]   CHARACTERIZATION OF MANUFACTURING EFFECTS FOR BUCKLING-SENSITIVE COMPOSITE CYLINDERS [J].
CHRYSSANTHOPOULOS, MK ;
GIAVOTTO, V ;
POGGI, C .
COMPOSITES MANUFACTURING, 1995, 6 (02) :93-101
[7]   Buckling and ultimate strength criteria of stiffened shells under combined loading for reliability analysis [J].
Das, PK ;
Thavalingam, A ;
Bai, Y .
THIN-WALLED STRUCTURES, 2003, 41 (01) :69-88
[8]  
GIAVOTTO V, 1991, BUCKLING OF SHELL STRUCTURES, ON LAND, IN THE SEA AND IN THE AIR, P53
[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 behavior of composite laminates with two delaminations under uniaxial compression [J].
Hwang, SF ;
Huang, SM .
COMPOSITE STRUCTURES, 2005, 68 (02) :157-165