[1] ZHOU Y Q, ZHU J S, GUO Y L. Numerical and experimental studies on sectional load capacity of concrete-infilled double steel corrugated-plate walls under combined compression and in-plane bending[J]. Thin-Walled Structures, 2021, 159: 107250. [2] WANG S H, HE J, LIU Y Q. Shear behavior of steel I-girder with stiffened corrugated web, Part Ⅰ: Experimental study[J]. Thin-Walled Structures, 2019, 140: 248-262. [3] 吴存利, 段世慧, 李新祥. 复合材料波纹板剪切载荷作用下的屈曲试验与分析[J]. 航空学报, 2011, 32(8): 1453-1460. [4] 吴存利, 段世慧, 孙侠生. 复合材料波纹板刚度工程计算方法及其在结构分析中的应用[J]. 航空学报, 2008, 29(6): 1570-1575. [5] 郑宇宁, 邱志平, 苑凯华. 复合材料波纹板在剪切载荷下的屈曲特性分析与可靠性优化[J]. 振动与冲击, 2016, 35(19): 7-25. [6] 秋洪燕, 矫桂琼, 黄涛. 复合材料层压梁梯形波纹腹板刚度和稳定性等效分析方法研究[J]. 机械强度, 2012, 34(6): 899-906. [7] 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. [8] 周春华, 王帮峰, 刘曌, 等. 波纹型复合材料蒙皮拉伸变形特性研究与仿真分析[J]. 科学技术与工程, 2011, 11(32): 7899-7930. [9] 周华志, 王志瑾, 韩微, 等. 具有褶皱薄弱段的正弦波纹梁吸能性能研究[J]. 振动与冲击, 2017, 36(17): 248-254. [10] 卢致龙, 常成. 直升机复合材料波纹梁结构抗坠毁设计技术研究[J]. 直升机技术, 2015, 185: 14-19. [11] REN Y R, JIANG H Y, JI W Y. Improvement of progressive damage model to predicting crashworthy composite corrugated plate[J]. Applied Composite Materials, 2018, 25: 45-66. [12] XIA Y, FRISWELL M I, SAAVEDRA E I. Equivalent models of corrugated panels[J]. International Journal of Solids and Structures, 2012, 49: 1453-1462. [13] WANG C, XIA Y, FRISWELL M I, et al. Predicting global strain limits for corrugated panels[J]. Composite Structures, 2020, 231:111472. [14] GOLZAR M, GHABEZI P. Corrugated composite skins[J]. Mechanics of Composite Materials, 2014, 50(2): 137-148. [15] NAHAS M N. Local buckling of composite corrugated compression panels[J]. Advanced Composite Materials, 1993, 3(1): 73-83. [16] GHABEZI P, GOLZAR M. Mechanical analysis of trapezoidal corrugated composite skins[J]. Applied Composite Materials, 2013, 20: 341-353. [17] GHABEZI P. Rectangular and triangular corrugated composite skins[J]. Fibers and Polymers, 2018, 19(2): 435-445. [18] JOACHIM L G, REANY J. Wrinkling of corrugated skin sandwich panels[J]. Composites Part A: Applied Science & Manufacturing, 2007, 38: 576-589. [19] PENG L X, LIEW K M, KITIPORNCHAI S. Analysis of stiffened corrugated plates based on the FSDT via the mesh-free method[J]. International Journal of Mechanical Science, 2007, 49: 364-378. [20] LIEW K M, PENG L X, KITIPORNCHAI S. Buckling analysis of corrugated plates using a mesh-free Galerkin method based on the first-order shear deformation theory[J]. Computational Mechanics, 2006, 38: 61-75. [21] YOKOZEKI T, TAKEDA S, OGASAWARA T, et al. Mechanical properties corrugated composites for candidate materials flexible wing structures[J]. Composites Part A: Applied Science & Manufacturing, 2006, 37: 1578-1586. [22] FILIPOVIC D T, KRESS G R. A planar finite element formulation for corrugated laminates under transverse shear loading[J]. Composite Structures, 2018, 201: 958-967. [23] PATHIRANA S, QIAO P Z. Local buckling analysis of periodic sinusoidal corrugated composite panels under uniaxial compression[J]. Composite Structures, 2019, 220: 148-157. [24] PATHIRANA S, QIAO P Z. Elastic local buckling of periodic sinusoidal corrugated composite panels[J]. Thin-Walled Structures, 2020, 157: 107134. [25] THURNHERR C, RUPPEN L, KRESS G R, et al. Interlaminar stresses in corrugated laminates[J]. Composite Structures, 2016, 140: 296-308. [26] FILIPOVIC D T, KRESS G R. Stress analysis of corrugated orthotropic laminates under transverse shear loading[J]. Composite Structures, 2019, 223: 110983. [27] FILIPOVIC D T, KRESS G R. A planar finite element formulation for corrugated laminates under transverse shear loading[J]. Composite Structures, 2018, 201: 958-967. [28] BAI J B, CHEN D, XIONG J J, et al. A corrugated flexible composite skin for morphing applications[J]. Composites Part B: Engineering, 2017, 131: 134-143. [29] LIU T W, BAI J B, LI S L, et al. Large deformation and failure analysis of the corrugated flexible composite skin for morphing wing[J]. Engineering Structures, 2023, 278: 115463. [30] SOLTANIA Z, HOSSEINI S A, KRESS G. Experimental and numerical study of geometrically nonlinear behavior of corrugated laminated composite shells using a nonlinear layer-wise shell FE formulation[J]. Engineering Structures, 2019, 184: 61-73. [31] ERMAKOVA A, DAYYANI I. Shape optimisation of composite corrugated morphing skins[J]. Composites Part B: Engineering, 2017, 115: 87-101. [32] 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: 132-133. [33] 高珂, 孙秦, 董文俊. 手风琴式蜂窝材料等效弯曲和扭转刚度分析[J]. 机械科学与技术, 2014, 33(10): 1579-1584. |