[1] 顾轶卓, 李敏, 李艳霞, 等. 飞行器结构用复合材料制造技术与工艺理论进展[J]. 航空学报, 2015, 36 (8): 2773-2797. [2] 马立敏, 张嘉振, 岳广全. 复合材料在新一代大型民用飞机中的应用[J]. 复合材料学报, 2015, 32(2): 317-322. [3] 中国民用航空局. 运输类飞机适航标准: CCAR25(R4)[S]. 北京: 2016. [4] LIU Q L, ZHAO Y. Prediction of natural frequencies of a sandwich panel using thick plate theory[J]. Journal of Sandwich Struct Mater, 2001, 3(4): 289-309. [5] LIU Q L, ZHAO Y. Effect of soft honeycomb core on flexural vibration of sandwich panel using low order and high order shear deformation models[J]. Journal of Sandwich Structures and Materials, 2007(9): 95-108. [6] RAO M K, DESAI Y M. Analytical solutions for vibrations of laminated and sandwich plates using mixed theory[J]. Composite Structures, 2004, 63: 361-373. [7] MOHAMED A A M, HADJ H A, ABDELOUAHAD T. An efficient and simple refined theory for buckling and free vibration of exponentially graded sandwich plates under various boundary conditions[J]. Journal of Sandwich Structures and Materials, 2014, 16(3): 293-318. [8] FIORENZO A F, ERASMO C. Free vibration analysis of sandwich plates with anisotropic face sheets in thermal environment by using the hierarchical trigonometric Ritz formulation[J]. Composites: Part B, 2013, 50: 67-81. [9] HIROYUKI M. Free vibration and stability of angle-ply laminated composite and sandwich plates under thermal loading[J]. Composite Structures, 2007, 77: 249-262. [10] LI X Y, YU K P, HAN J Y, et al. A piecewise shear deformation theory for free vibration of composite and sandwich panels[J]. Composite Structures, 2015, 124: 111-119. [11] LI X Y, YU K P. Vibration and acoustic responses of composite and sandwich panels under thermal environment[J]. Composite Structures, 2015, 131: 1040-1049. [12] ZHAO R, YU K P, GREGORY M H, et al. Piecewise shear deformation theory and finite element formulation for vibration analysis of laminated composite and sandwich plates in thermal environments[J]. Composite Structures, 2017, 160: 1060-1083. [13] 吴大方, 王岳武, 蒲颖, 等. 高超声速飞行器复合材料翼面结构1100℃高温环境下的热模态试验[J]. 复合材料学报, 2015, 32(2): 323-331. [14] 东巳宙. 高温环境下复合材料层合板与蜂窝板力学性能分析[D]. 哈尔滨: 哈尔滨工业大学, 2016. [15] BAI Y H, YU K P, ZHAO J, et al. Experimental and simulation investigate on of temperature effects on modal characteristics of composite honeycomb structure[J]. Composite Structures, 2018, 201: 816-827. [16] 贾宝惠, 郝彤星, 张刚, 等. 湿热环境对复合材料蜂窝板振动特性的影响[J]. 复合材料学报, 2020, 37(7): 1601-1610. [17] KWON Y W, LANNAMANN D L. Dynamic numerical modeling and simulation of interfacial cracks in sandwich structures for damage detection[J]. Journal of Sandwich Structures and Materials, 2002(4): 175-199. [18] KIM H Y, HWANG W B. Effect of debonding on natural frequencies and frequency response functions of honeycomb sandwich beams[J]. Composite Structures, 2002, 55: 51-62. [19] BABA B O, THOPPUL S. Experimental evaluation of the vibration behavior of flat and curved sandwich composite beams with face/core debond[J]. Composite Structures, 2009, 91: 110-119. [20] PARK Y B, KWEON J H, CHOI J H. Failure characteristics of carbon/BMI-Nomex sandwich joints in various hygrothermal conditions[J]. Composites: Part B, 2014, 60: 213-221. [21] FARSHIDIA A, BERGGREENA C, SCHAUBLE R. Numerical fracture analysis and model validation for disbonded honeycomb core sandwich composites[J]. Composite Structures, 2019, 210: 231-238. [22] 蒋莉, 张志民. 湿热问题全复合材料夹层板面芯分层屈曲研究[J]. 北京航空航天大学学报, 2002, 28: 438-442. [23] 贾宝惠, 张刚, 蔺越国, 等. 湿热环境下含分层平面编织玻璃纤维/环氧树脂基复合材料层合板振动特性[J]. 复合材料学报, 2019, 36(4): 892-904. [24] ZHU K G, CHEN M J, LU Q H, et al. Debonding detection of honeycomb sandwich structures using frequency response functions[J]. Journal of Sound and Vibration, 2014, 333: 5299-5311. [25] 白云鹤, 于开平, 赵锐, 等. 高温与脱粘对复合材料蜂窝板模态特性影响的试验[J]. 复合材料学报, 2018, 35(4): 885-895. [26] 赵天, 杨智春, 田玮, 等. 湿热环境下复合材料层合板振动与声辐射特性分析[J]. 航空学报, 2017, 38(10): 144-154. [27] JIANG D, ZHANG D H, FEI Q G, et al. An approach on identifi-cation of equivalent properties of honeycomb core using experimental modal data[J]. Finite Elements in Analysis and Design, 2014, 90: 84-92. |