复合材料曲板缺陷及安装误差对屈曲性能的影响

doi:10.7527/S1000-6893.2015.0352

Abstract

Abstract:

Buckling behavior of composite curved panels is sensitive to defects. Studies of the effects of defects on buckling performance in numerical simulations and tests are of great significance to engineering applications of composite curved panels. The effects of common defects in composite cylindrical panels and fix-errors caused by these defects on buckling behavior are studied by numerical simulations. Ideal curved panels and panels with defects are modeled and fix-errors caused by defects are considered. The defects occasionally come from manufacturing process, including inclination, non-uniform thickness and warpage. Bulking loads and strain distribution of curved panels are calculated. Results of panels with defects are compared with those of ideal curved panels. The research indicates that inclination has a great influence on the strain distribution of loaded panels, which makes critical buckling loads decrease sharply. Warpage has fewer effects on the strain distribution but also makes critical buckling loads decrease greatly. Non-uniform thickness has little effect on buckling behavior of cylindrical panels. Experiment of panels with defects under axial uniform load is carried out and testing results verify the numerical results.

Key words: cylindrical panel, buckling, defects, fix-errors, FEA

CLC Number:

V214.8
TB332

ZHU Lin, YU Yin, WANG Hai. Effects of defects in cylindrical panels and fix-errors on buckling behavior[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2016, 37(7): 2180-2188.

References

[1] REDSHAW S C. The elastic instability of a thin curved panel subjected to an axial thrust, its axial and circumferential edges being simply supported[R]. Greenwich:Bristish Aeronautical Research Council, 1934.
[2] TIMOSHENKO S P, GERE J M. Theory of elastic stability[M]. New York:McGraw-Hill, 1961:462-468.
[3] GERARD G, BECKER H. Handbook of structural stability Part Ⅲ:Buckling of curved plates and shells:NACA TN 3783[R]. Washington, D.C.:NASA, 1957.
[4] LE TRAN K, DAVAINE L, DOUTHE C, et al. Stability of curved panels under uniform axial compression[J]. Journal of Constructional Steel Research, 2012, 69(1):30-38.
[5] MARTINS J P, DA SILVA L S, REIS A. Eigenvalue analysis of cylindrically curved panels under compressive stresses-Extension of rules from EN 1993-1-5[J]. Thin-Walled Structures, 2013, 68:183-194.
[6] MARTINS J P, BEG D, SINUR F, et al. Imperfection sensitivity of cylindrically curved steel panels[J]. Thin-Walled Structures, 2015, 89:101-115.
[7] SHARIATI M. A numerical and experimental study on buckling of cylindrical panels subjected to compressive axial load[J]. Strojniški Vestnik-Journal of Mechanical Engineering, 2010, 56(10):609-618.
[8] WILKINS D J. Compression buckling tests of laminated graphite-epoxy curved panels[J]. AIAA Journal, 1975, 13(4):465-470.
[9] SHEN H S. Hygrothermal effects on the postbuckling of axially loaded shear deformable laminated cylindrical panels[J]. Composite Structures, 2002, 56(1):73-85.
[10] ZIMMERMANN R, KLEIN H, KLING A. Buckling and postbuckling of stringer stiffened fiber composite curved panels-Tests and computations[J]. Composite Structures, 2006, 73(2):150-161.
[11] VESCOVINI R, BISAGNI C. Buckling analysis and optimization of stiffened composite flat and curved panels[J]. AIAA Journal, 2012, 50(4):904-915.
[12] LI C, WU Z. Buckling of 120° stiffened composite cylindrical shell under axial compression-Experiment and simulation[J]. Composite Structures, 2015, 128:199-206.
[13] 张劲松, 余音, 汪海. 二维编织复合材料圆柱曲板屈曲性能试验与有限元分析[J]. 复合材料学报, 2015, 32(3):805-814. ZHANG J S, YU Y, WANG H. Test and finite element analysis of buckling performance for 2D textile composite cylindrical curved panels[J]. Acta Materiae Composite Sinica, 2015, 32(3):805-814(in Chinese).
[14] 卢文书, 马元春, 梁伟, 等. 机身复合材料加筋板壳的稳定性及强度分析系统[J]. 航空学报, 2009, 30(5):895-900. LU W S, MA Y C, LIANG W, et al. Analysis system of stability and strength for airframe composite stiffened plate/shell[J]. Acta Aeronautica et Astronautica Sinica, 2009, 30(5):895-900(in Chinese).
[15] ARBOCZ J. Post-buckling behaviour of structures numerical techniques for more complicated structures[M]. Heidelberg:Springer Berlin Heidelberg, 1987:84-142.
[16] 《飞机设计手册》总编委会.飞机设计手册第9册. 载荷、强度和刚度[M]. 北京:航空工业出版社, 2001:436-437. Editorial Committee of Aircraft Design Handbook. Aircraft design handbook, Section 9:Load, strength and stiffness[M]. Beijing:Aviation Industry Press, 2001:436-437(in Chinese).
[17] 崔德刚. 结构稳定性设计手册[M]. 北京:航空工业出版社, 1996:64-66. CUI D G. Structure stability design manual[M]. Beijing:Aviation Industry Press, 1996:64-66(in Chinese).
[18] 中国航空研究院. 复合材料结构稳定性分析指南[M]. 北京:航空工业出版社, 2002:6-7. Chinese Aeronautical Establishment. Composite structure stability analysis guidance[M]. Beijing:Aviation Industry Press, 2002:6-7(in Chinese).
[19] 朱菊芬, 汪海, 徐胜利. 非线性有限元及其在飞机结构设计中的应用[M]. 上海:上海交通大学出版社,2012:121-123. ZHU J F, WANG H, XU S L. Nonlinear finite element method and applications in aircraft structure design[M]. Shanghai:Shanghai Jiao Tong University Press, 2012:121-123(in Chinese).
[20] 孙璐妍, 余音, 陈博, 等. 一种新的柱形曲板轴压屈曲试验四边简支边界的实现方法[J]. 机械工程学报, 2014, 50(8):53-58. SUN L Y, YU Y, CHEN B, et al. A new method for implementation of simple supported boundary in stability test of cylindrical panel under axial compression[J]. Journal of Mechanical Engineering, 2014, 50(8):53-58(in Chinese).
[21] 孙璐妍, 余音, 汪海. 用于柱形曲板轴压稳定性试验的固定夹具:CN203037527U[P]. 2013-07-03. SUN L Y, YU Y, WANG H. A fixture for axial compression stability test of cylindrical panels:CN-203037527U[P]. 2013-07-03(in Chinese).

Effects of defects in cylindrical panels and fix-errors on buckling behavior

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