| Citation: | WANG C S，ZHANG X Y，ZHAN Z X，et al. Analysis of compression stability and load capacity of thick composite plate structures[J]. Journal of Beijing University of Aeronautics and Astronautics，2025，51（1）：94-101 （in Chinese） doi: 10.13700/j.bh.1001-5965.2022.0991
|
The compression stability of composite thick plates was studied. Firstly, the compression test was carried out on the thick plate structure of the composite fuselage. It was found that the bottom skin of the stringer was buckling first, and the stringer did not play the role of wave isolation. Secondly, the finite element linear and nonlinear analysis methods were carried out on the structure. The he buckling characteristics was verified. Finally, the stability analysis method was revised according to the test and analysis results. The buckling load and bearing capacity calculated by the modified analysis method were more accurate. A new method for buckling analysis and load-bearing capacity calculation of composite thick plate structures was established.
| [1] |
KASSAPOGLOU C. Design and analysis of composite structures[M]. New York: Wiley, 2013: 237-273.
|
| [2] |
王菲菲, 崔德刚, 熊强, 等. 复合材料加筋板后屈曲承载能力工程分析方法[J]. 北京亚洲成人在线一二三四五六区学报, 2013, 39(4): 494-497.
WANG F F, CUI D G, XIONG Q, et al. Engineering analysis of post-buckling loading capability for composite stiffened panels[J]. Journal of Beijing University of Aeronautics and Astronautics, 2013, 39(4): 494-497(in Chinese).
|
| [3] |
李乐坤, 李曙林, 常飞, 等. 复合材料加筋壁板压缩屈曲与后屈曲分析[J]. 南京亚洲成人在线一二三四五六区学报, 2016, 48(4): 563-568.
LI L K, LI S L, CHANG F, et al. Buckling and post-buckling of composite stiffened panel under compression[J]. Journal of Nanjing University of Aeronautics & Astronautics, 2016, 48(4): 563-568(in Chinese).
|
| [4] |
谭翔飞, 何宇廷, 冯宇, 等. 航空复合材料加筋板剪切稳定性及后屈曲承载性能[J]. 复合材料学报, 2018, 35(2): 320-331.
TAN X F, HE Y T, FENG Y, et al. Stability and post-buckling carrying capacity of aeronautic composite stiffened panel under shear loading[J]. Acta Materiae Compositae Sinica, 2018, 35(2): 320-331(in Chinese).
|
| [5] |
高志刚, 冯宇, 马斌麟, 等. 航空复合材料加筋板压缩屈曲及后屈曲力学性能[J]. 航空材料学报, 2020, 40(1): 53-61.
GAO Z G, FENG Y, MA B L, et al. Compressive bucking and post-bucking mechanical properties of aeronautic composite stiffened panel[J]. Journal of Aeronautical Materials, 2020, 40(1): 53-61(in Chinese).
|
| [6] |
王彬文, 张长兴, 郭文杰, 等. 考虑屈曲的复合材料加筋壁板铺层顺序优化[J]. 复合材料学报, 2021, 38(12): 4123-4137.
WANG B W, ZHANG C X, GUO W J, et al. Stacking sequence optimization of composite stiffened panel considering buckling[J]. Acta Materiae Compositae Sinica, 2021, 38(12): 4123-4137(in Chinese).
|
| [7] |
王燕, 李书, 许秋怡, 等. 复合材料加筋板剪切后屈曲分析与优化设计[J]. 航空学报, 2016, 37(5): 1512-1525.
WANG Y, LI S, XU Q Y, et al. Optimization design and analysis of stiffened composite panels in post-buckling under shear[J]. Acta Aeronautica et Astronautica Sinica, 2016, 37(5): 1512-1525(in Chinese).
|
| [8] |
STAMATELOS D G, LABEAS G N, TSERPES K I. Analytical calculation of local buckling and post-buckling behavior of isotropic and orthotropic stiffened panels[J]. Thin-Walled Structures, 2011, 49(3): 422-430. doi: 10.1016/j.tws.2010.11.008
|
| [9] |
BACCIOCCHI M, TARANTINO A M. Analytical solutions for vibrations and buckling analysis of laminated composite nanoplates based on third-order theory and strain gradient approach[J]. Composite Structures, 2021, 272: 114083. doi: 10.1016/j.compstruct.2021.114083
|
| [10] |
DHURVEY P, MITTAL N D. Buckling behavior of an orthotropic composite laminate using finite element analysis[J]. International Journal of Scientific Engineering and Technology, 2012, 1(4): 93-95.
|
| [11] |
PAIK J K, SEO J K. Nonlinear finite element method models for ultimate strength analysis of steel stiffened-plate structures under combined biaxial compression and lateral pressure actions—Part II: Stiffened panels[J]. Thin-Walled Structures, 2009, 47(8-9): 998-1007. doi: 10.1016/j.tws.2008.08.006
|
| [12] |
TAKANO A. Buckling test of CFRP cylindrical shells under compression load[J]. Journal of the Japan Society for Aeronautical and Space Sciences, 2018, 66(4): 98-111. doi: 10.2322/jjsass.66.98
|
| [13] |
石经纬, 赵娟, 刘传军, 等. 复合材料翼面壁板轴压稳定性[J]. 复合材料学报, 2020, 37(6): 1321-1333.
SHI J W, ZHAO J, LIU C J, et al. Stability of composite stiffened panels under compression[J]. Acta Materiae Compositae Sinica, 2020, 37(6): 1321-1333(in Chinese).
|
| [14] |
万华亮, 龚伟明, 覃俊娥. 复合材料帽型加筋壁板轴压稳定性研究[J]. 强度与环境, 2019, 46(1): 31-34.
WAN H L, GONG W M, QIN J E. Research on the buckling and post-buckling behavior of hat-stiffened composite panels under axial compressive load[J]. Structure & Environment Engineering, 2019, 46(1): 31-34(in Chinese).
|
| [15] |
葛建彪. 复合材料加筋壁板稳定性及承载能力分析[D]. 南京: 南京亚洲成人在线一二三四五六区, 2010.
GE J B. Stability and bearing capacity analysis of composite stiffened panel[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2010(in Chinese).
|
| [16] |
STEVENS K A, RICCI R, DAVIES G A O. Buckling and postbuckling of composite structures[J]. Composites, 1995, 26(3): 189-199. doi: 10.1016/0010-4361(95)91382-F
|
| [17] |
KONG C W, LEE I C, KIM C G, et al. Postbuckling and failure of stiffened composite panels under axial compression[J]. Composite Structures, 1998, 42(1): 13-21. doi: 10.1016/S0263-8223(98)00044-0
|
| [18] |
SHI G, XIONG Y. Probabilistic buckling analysis of fiber metal laminates under shear loading condition[J]. Advances in Engineering Software, 2000, 31(8): 519-527.
|
| [19] |
MISHRA B B, KUMAR A, SAMUI P, et al. Buckling of laminated composite skew plate using FEM and machine learning methods[J]. Engineering Computations, 2021, 38(1): 501-528. doi: 10.1108/EC-08-2019-0346
|
| [20] |
VON KÁRMÁN T, TSIEN H S. The buckling of thin cylindrical shells under axial compression[M]. Amsterdam: Elsevier, 2012: 165-181.
|
| [21] |
STEIN M. Some recent advances in the investigation of shell buckling[J]. AIAA Journal, 1968, 6(12): 2339-2345. doi: 10.2514/3.4992
|
| [22] |
李真, 王俊, 邓凡臣, 等. 复合材料机身壁板的强度分析与试验验证[J]. 航空学报, 2020, 41(9): 118-130.
LI Z, WANG J, DENG F C, et al. Strength analysis and test verification of composite fuselage panels[J]. Acta Aeronautica et Astronautica Sinica, 2020, 41(9): 118-130(in Chinese).
|
| [23] |
陈庆远. 复合材料薄壁结构的屈曲和后屈曲分析[D]. 上海: 上海交通大学, 2015.
CHEN Q Y. Buckling and post-buckling analysis of composite thin-walled structures[D]. Shanghai: Shanghai Jiao Tong University, 2015(in Chinese).
|
| [24] |
LI Z C, XIE Y G. Buckling mechanism of thin-walled arches with composite polyhedral shapes[J]. Composite Structures, 2021, 271: 114134. doi: 10.1016/j.compstruct.2021.114134
|
| [25] |
EINAFSHAR N, LEZGY-NAZARGAH M, BEHESHTI-AVAL S B. Buckling, post-buckling and geometrically nonlinear analysis of thin-walled beams using a hypothetical layered composite cross-sectional model[J]. Acta Mechanica, 2021, 232(7): 2733-2750. doi: 10.1007/s00707-021-02936-3
|
| [26] |
CHANG K, JENSEN J, MATTHEWS R, et al. Buckling strength of carbon/carbon panels[C]//Proceedings of the 31st Structures, Structural Dynamics and Materials Conference. Reston: AIAA, 1990.
|
| [27] |
王勖成. 有限单元法[M]. 北京: 清华大学出版社, 2003: 649-651.
WANG X C. Finite element method[M]. Beijing: Tsinghua University Press, 2003: 649-651(in Chinese).
|
| [28] |
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: 5-11.
China Aviation Research Institute. Guide to structural stability analysis of composite materials[M]. Beijing: Aviation Industry Press, 2002: 5-11(in Chinese).
|
| [29] |
VON KÁRMÁN T, SECHLER E E, DONNELL L H. The strength of thin plates in compression[J]. Journal of Fluids Engineering, 1932, 54(2): 53-56.
|
| [30] |
牛春匀. 实用飞机结构应力分析及尺寸设计[M]. 冯振宇, 程小全, 张纪奎, 译. 北京: 航空工业出版社, 2009: 394-395.
NIU C Y. Airframe stress analysis and sizing[M]. FENG Z Y, CHENG X Q, ZHANG J K , Translated. Beijing: Aviation Industry Press, 2009: 394-395(in Chinese).
|
Figures(16) / Tables(4)
Copyright © Journal of Beijing University of Aeronautics and Astronautics
Address: Editorial Department of Journal of Beijing University of Aeronautics and Astronautics, 37 Xueyuan Road, Haidian District, Beijing Post Code: 100191 Email: jbuaa@cqjj8.com
Supported by:
Beijing Renhe Information Technology Co., Ltd.
DownLoad:
