全复合材料波纹夹芯圆柱壳轴压屈曲行为解析预测

doi:10.19936/j.cnki.2096-8000.20260428.014

复合材料科学与工程 ›› 2026, Vol. 0 ›› Issue (4): 115-123.DOI: 10.19936/j.cnki.2096-8000.20260428.014

全复合材料波纹夹芯圆柱壳轴压屈曲行为解析预测

周文婷¹, 王从¹, 王艳霞², 马苗立³

1.石家庄理工职业学院智能制造与技术学院,石家庄 050228;
2.石家庄铁道大学交通运输学院,石家庄 050043;
3.北京石油化工学院信息工程学院,北京 102627

收稿日期:2025-11-17 发布日期:2026-06-16
作者简介:周文婷(1990—),女,硕士,讲师,主要从事复合材料力学与结构设计方面的研究,zwt08220@ 163.com。
基金资助:
河北省重大科技支撑计划项目(252Y5401D)

Analytical prediction of axial compression buckling behavior of all-composite corrugated sandwich cylindrical shell

ZHOU Wenting¹, WANG Cong¹, WANG Yanxia², MA Miaoli³

1. School of Intelligent Manufacturing and Technology, Shijiazhuang Institute of Technology, Shijiazhuang 050228, China;
2. School of Traffic and Transportation, Shijiazhuang Tiedao University, Shijiazhuang 050043, China;
3. School of Information Engineering, Beijing Institute of Petrochemical Technology, Beijing 102627, China

Received:2025-11-17 Published:2026-06-16

摘要/Abstract

摘要： 针对全复合材料纵向连续梯形波纹圆柱壳轴压线性屈曲行为,提出便于工程应用的解析预测方法。该方法计算分析效率高,能区分胞元间面板屈曲、波纹腹板屈曲、夹芯壁板屈曲和圆柱壳整体屈曲等4种屈曲失稳模式,对应计算出的屈曲临界应力与三维有限元仿真结果的误差在±12%以内。基于验证过的解析公式开展参数分析,协同分析了复合材料波纹夹芯圆柱壳屈曲临界应力和失稳模式随结构、铺层参数的变化规律,绘制了失稳机制图。研究发现:全复合材料波纹夹芯圆柱壳不易发生夹芯壁板屈曲,增大波纹倾斜角度或芯子壁板厚度能提高屈曲临界应力;保持所有几何尺寸不变,屈曲临界应力和失稳模式会随面板、芯子铺层角度的变化而变化,胞元间面板屈曲临界应力和波纹腹板屈曲临界应力均在45°时达到极值。

关键词: 复合材料, 波纹夹芯圆柱壳, 屈曲临界应力, 屈曲失稳模式, 失稳机制

Abstract: For the axial linear buckling behavior of all-composite longitudinally continuous trapezoidal corrugated the cylindrical shell, an analytical prediction method convenient for engineering application was proposed. This method was highly efficient for calculation and analysis, and could distinguish four buckling instability modes: intracellular face buckling, corrugation buckling, sandwich panel buckling and cylindrical shell global buckling. The errors between the calculated critical buckling stress and the 3D finite element simulation results were within ±12%. Based on the validated analytical formulas, parameters analysis were conducted to collaboratively analyze the variations of buckling critical stress, instability modes of the composite corrugated sandwich cylindrical shell with structural and layup parameters, and failure mechanism diagrams were drawn. It is found that all-composite corrugated sandwich cylindrical shells are not prone to sandwich panel buckling; increasing the corrugation inclination angle or the thickness of the wall of the core can improve the buckling critical stress; with all geometric dimensions unchanged, buckling critical stress and instability modes also vary with the ply angles of the face and the core, and the critical stress of intracellular face buckling and of corrugation buckling reach their extreme values at 45°.

Key words: composite materials, corrugated sandwich cylindrical shell, critical buckling stress, buckling instability mode, instability mechanism

中图分类号:

TB332

周文婷, 王从, 王艳霞, 马苗立. 全复合材料波纹夹芯圆柱壳轴压屈曲行为解析预测[J]. 复合材料科学与工程, 2026, 0(4): 115-123.

ZHOU Wenting , WANG Cong , WANG Yanxia , MA Miaoli. Analytical prediction of axial compression buckling behavior of all-composite corrugated sandwich cylindrical shell[J]. COMPOSITES SCIENCE AND ENGINEERING, 2026, 0(4): 115-123.

参考文献

[1] 王文煜, 李锋, 任飞翔, 等. 轻质高强复合材料网格加筋壳体结构设计方法及力学性能研究进展[J]. 航空学报, 2024, 45(17): 99-116.
[2] 熊健, 李志彬, 刘惠彬, 等. 航空航天轻质复合材料壳体结构研究进展[J]. 复合材料学报, 2021, 38(6): 1629-1650.
[3] 梁泽乾, 魏刚, 李想. 复合材料纵向圆形波纹圆柱壳轴向压缩失效特性研究[J]. 复合材料科学与工程, 2023(5): 45-52, 70.
[4] XIONG J, FEND L N, GHOSH R, et al. Fabrication and mechanical behavior of carbon fiber composite sandwich cylindrical shellswith corrugated cores[J]. Composite Structures, 2016, 156: 307-319.
[5] 冯丽娜, 熊健, 郑伟, 等. 复合材料波纹夹层圆柱壳设计及轴压性能[J]. 复合材料学报, 2016, 33(2): 418-429.
[6] GU F W, CHEN L, ZHU X L, et al. Fabrication and uniaxial compression mechanical behavior of composite corrugated-core sandwich cylinder with thin-wall metal liner[J]. Mechanics of Advanced Materials and Structures, 2022, 29(7): 949-962.
[7] FAN H L, FANG D N, CHEN L M, et al. Manufacturing and testing of a CFRC sandwich cylinder with Kagome cores[J]. Composites Science and Technology, 2009, 69(15/16): 2695-2700.
[8] LI Z B, GAO Y, XU P P, et al. Fabrication and failure mechanisms of all-composite honeycomb sandwich cylinder under the axial compression[J]. Composites Part A: Applied Science and Manufacturing, 2022, 161: 107075.
[9] 陈悦, 朱锡, 李华东, 等. 轴压作用下缠绕复合材料夹芯圆柱壳力学性能研究[J]. 玻璃钢/复合材料, 2016(7): 5-8.
[10] LIU B, SUN Y G, SUN Y, et al. Fabrication and compressive behavior of carbon-fiber-reinforced cylindrical foldcore sandwich structure[J]. Composites Part A:Applied Science and Manufacturing, 2018, 118: 9-19.
[11] 李泽成, 吴健, 王纬波. 内外压力作用下复合材料夹芯圆柱壳的屈曲及面芯分层扩展研究[J]. 船舶力学, 2018, 22(10): 1233-1240.
[12] WEAVER P M. Design of laminated composite cylindrical shells under axial compression[J]. Composites Part B: Engineering, 2000, 31(8): 669-679.
[13] LI W X, SUN F F, WEI W Y, et al. Fabrication and testing of composite corrugated-core sandwich cylinder[J]. Composites Science and Technology, 2018, 156: 127-135.
[14] JIANG S, SUN F F, FAN H L. Multi-failure theory of composite orthogrid sandwich cylinder[J]. Aerospace Science and Technology, 2017, 70: 520-525.
[15] 罗培林. 强度稳定综合理论[M]. 北京: 科学出版社, 2014: 52-62.
[16] 朱锐杰, 李峰, 张恒铭. 基于弹性基础梁理论的复合材料薄壁圆柱壳屈曲承载力模型[J]. 复合材料学报, 2017, 34(8): 1745-1753.
[17] KOLLÁ L P, et al. Local buckling of fiber reinforced plastic composite structural members with open and closed cross sections[J]. Journal of Structural Engineering, 2003, 129(11): 1503-1513.
[18] KOLLÁ L P, et al. Buckling of unidirectionally loaded composite plates with one free and one rotationally restrained unloaded edge[J]. Journal of Structural Engineering, 2002, 128(9): 1202-1211.
[19] 陈烈民, 杨宝宁. 复合材料的力学分析[M]. 北京: 中国科学技术出版社, 2006: 241-258.
[20] ZHU X J, XIONG C, YIN J H, et al. Equivalent stiffness prediction and global buckling analysis using refined analytical model of composite laminated box beam[J]. Science and Engineering of Composite Materials, 2019, 26(1): 465-481.
[21] ZHU X J, XIONG C, YIN J H, et al. Bending responses of CFRP thin-walled tubes with different sectional shapes: experimental, analytical and numerical investigation[J]. Composite Structures, 2023, 304: 116374.

全复合材料波纹夹芯圆柱壳轴压屈曲行为解析预测

Analytical prediction of axial compression buckling behavior of all-composite corrugated sandwich cylindrical shell

PDF (PC)

可视化

摘要/Abstract

引用本文

使用本文

参考文献

相关文章 15

编辑推荐

Metrics

本文评价

[1]	赵彦淇, 戴勇, 刘畅, 来晓靓, 孙成, 刘小林, 邵纯. 温度对新型航空复合材料IMA/M21X力学性能影响的试验研究[J]. 复合材料科学与工程, 2026, 0(4): 1-8.
[2]	张耀之, 徐锦文, 赵星诺, 蒋峰光, 束长朋, 周权. 硅炔杂化树脂及其复合材料的制备与性能研究[J]. 复合材料科学与工程, 2026, 0(4): 9-17.
[3]	高龙威, 白一峰, 蒋金华, 陈南梁, 邵慧奇. 三维间隔织物混杂增强复合材料抗冲击性能研究[J]. 复合材料科学与工程, 2026, 0(4): 18-26.
[4]	马铭泽, 熊欣, 孟庆春, 吴富强, 赵亚盼, 乔巍. 复合材料层合板剪切非线性行为的试验及数值仿真研究[J]. 复合材料科学与工程, 2026, 0(4): 27-35.
[5]	丁慧, 刘庆辉, 乔丕忠. 卷边加筋肋约束下正交各向异性板剪切屈曲荷载的近似公式[J]. 复合材料科学与工程, 2026, 0(4): 36-43.
[6]	秦塬, 周进节, 彭志康. 基于自适应聚类与语义加权的空气耦合兰姆波无基准损伤成像方法[J]. 复合材料科学与工程, 2026, 0(4): 44-54.
[7]	刘国春, 沈赫, 孙华伟. 复合材料泡沫夹层结构非穿透损伤修理的四点弯曲性能研究[J]. 复合材料科学与工程, 2026, 0(4): 63-71.
[8]	张广滨, 李远辰, 李澳, 郑炎钊, 梁凯, 郭义. 多颗磨粒异步刻划C/SiC复合材料的三维多相有限元建模与试验研究[J]. 复合材料科学与工程, 2026, 0(4): 89-100.
[9]	陈新宇, 余敬升, 谌顺心, 徐任信. 铝合金表面协同处理及其与CF/PEEK板的电阻焊接研究[J]. 复合材料科学与工程, 2026, 0(4): 101-106.
[10]	贾宝惠, 周家星, 肖海建, 任鹏. 基于贝叶斯理论的湿热环境下含孔层合板剩余强度预测[J]. 复合材料科学与工程, 2026, 0(4): 107-114.
[11]	刘世宇, 牛雪娟. 基于响应面法复合材料固化变形影响研究[J]. 复合材料科学与工程, 2026, 0(4): 124-131.
[12]	马元春, 闫丽, 耿小亮, 张恒. 单向纤维铺缝复合材料单轴拉伸性能试验及模拟研究[J]. 复合材料科学与工程, 2026, 0(4): 132-137.
[13]	王晓文, 孙婕, 赵大娟, 王芸铖, 董继萍, 周正亮. 碳纤维中空织物复合材料的树脂缓释工艺研究[J]. 复合材料科学与工程, 2026, 0(4): 138-143.
[14]	胡玉杰, 曾永红, 刘永红, 孙琳, 张联合, 朱洪强, 路文凤, 蔡雅迪, 朱敏江, 周泽文, 张辉. 碳纤维增强树脂基复合材料拉挤成型工艺研究进展[J]. 复合材料科学与工程, 2026, 0(4): 144-160.
[15]	赵卫锋, 文嘉鑫, 周靖, 陈凯亮, 补国斌. GFRP-竹胶板管复合约束含砖骨料再生混凝土叠合柱抗压性能试验[J]. 复合材料科学与工程, 2026, 0(3): 10-20.