Citation: | AN Zejun, CAO Dongfeng, ZHENG Kaidong, et al. Effect of drilling delamination on compressive mechanical behaviour of open-hole laminates[J]. Acta Materiae Compositae Sinica, 2022, 39(6): 2974-2986. doi: 10.13801/j.cnki.fhclxb.20210902.005 |
[1] |
FREITAS M D, CARVALHO R D. Residual strength of a damaged laminated CFRP under compressive fatigue stresses[J]. Composites Science & Technology,2006,66(3-4):373-378.
|
[2] |
TAFRESHI A, OSWALD T. Global buckling behaviour and local damage propagation in composite plates with embedded delaminations[J]. International Journal of Pressure Vessels& Piping,2003,80(1):9-20.
|
[3] |
AUERSCH L, SCHMID G. A torque and thrust prediction model for drilling of composite materials[J]. Composites Part A: Applied Science & Manufacturing,2005,36(1):83-93.
|
[4] |
KHASHABA U A, EL-SONBATY I A, SELMY A I, et al. Machinability analysis in drilling woven GFR/epoxy composites: Part I-Effect of machining parameters[J]. Composites Part A: Applied Science & Manufacturing,2010,41(3):391-400.
|
[5] |
DUAN Q F, LI S X, SONG P H, et al. Effect of drilling-induced delamination on buckling behavior of open hole composite laminate specimens under compressive loading[J]. Strength of Materials,2019,51:624-632.
|
[6] |
HAN P K, WHITEHEAD R S, KAUTZ E F. Damage tolerance certification methodology for composite structures[C]. Eighth DOD(NASA)FAA Conference on Fibrous Compo-sites in Structural Design, Part 2. NASA. Langley Research Center, 1990.
|
[7] |
MCGOWAN D M, AMBUR D R. Structural response of composite sandwich panels impacted with and without compression loading[J]. Journal of Aircraft,1971,36(3):596-602.
|
[8] |
KARIMI N Z, HEIDARY H, FOTOUHI M, et al. Experimental analysis of GFRP laminates subjected to compression after drilling[J]. Composite Structures, 2017, 169: 144–152.
|
[9] |
OLSSON R. Analytical prediction of large mass impact damage in composite laminates[J]. Composites Part A: Applied Science & Manufacturing,2001,32(9):1207-1215.
|
[10] |
王雪明, 谢富原, 李敏, 等. 热压罐成型复合材料复杂结构对制造缺陷的影响规律[J]. 航空学报, 2009, 30(4):757-762. doi: 10.3321/j.issn:1000-6893.2009.04.029
WANG Xueming, XIE Fuyuan, LI Min, et al. Effect of complex structure on manufacturing defects of composite materials formed by auto-claves[J]. Acta Aeronautica et Astronautica Sinica,2009,30(4):757-762(in Chinese). doi: 10.3321/j.issn:1000-6893.2009.04.029
|
[11] |
KATERELOS D G, PAIPETIS A, KOSTOPOULOS V. A simple model for the prediction of the fatigue delamination growth of impacted composite panels[J]. Fatigue & Fracture of Engineering Materials& Structures,2004,27(10):911-922.
|
[12] |
ISMAIL S O, OJO S O, DHAKAL H N. Thermo-mechanical modelling of FRP cross-ply composite laminates drilling: Delamination damage analysis[J]. Composites Part B: Engineering,2017,108:45-52. doi: 10.1016/j.compositesb.2016.09.100
|
[13] |
张明辉, 周储伟, 鲁浩. 碳纤维复合材料单向板钻孔分层损伤的数值模拟[J]. 机械工程材料, 2019, 43(9):73-77.
ZHANG Minghui, ZHOU Chuwei, LU Hao. Numerical simulation of delamination dam-age of carbon fiber composite plate in borehole[J]. Materials for Mechanical Engineering,2019,43(9):73-77(in Chinese).
|
[14] |
唐荆, 陈啸, 杨科. 碳纤维复合材料开孔层合板压缩损伤预测和模型比较[J]. 玻璃钢/复合材料, 2019(10):33-39.
TANG Jing, CHEN Xiao, YANG Ke. Compression damage prediction and model comparison of carbon fiber compo-site open-hole laminates[J]. Fiber Reinforced Plastics/Composites,2019(10):33-39(in Chinese).
|
[15] |
温泉, 郭东明, 高航, 等. 碳纤维/环氧树脂复合材料制孔损伤综合评价方法[J]. 复合材料学报, 2016, 33(2):265-272.
WEN quan, GUO Dongming, GAO Hang, et al. Comprehensive evaluation method for hole damage of carbon fiber/epoxy resin composites[J]. Acta Materiae Compositae Sinica,2016,33(2):265-272(in Chinese).
|
[16] |
卓越, 关志东, 周睿, 等. 复合材料开孔层板压缩渐进损伤试验[J]. 复合材料学报, 2015, 32(6):1762-1768.
ZHUO Yue, GUAN Zhidong, ZHOU Rui, et al. Experimental study on progressive damage of composite laminates by compression[J]. Acta Materiae Compositae Sinica,2015,32(6):1762-1768(in Chinese).
|
[17] |
OJO S O, ISMAIL S O, PAGGI M, et al. A new analytical critical thrust force model for delamination analysis of laminated composites during drilling operation[J]. Composites Part B: Engineering, 2017, 124: 207–217.
|
[18] |
姜晓伟, 朱书华, 李国弘, 等. 含分层缺陷复合材料层合板分层扩展研究[J]. 航空计算技术, 2014, 44(5):73-76. doi: 10.3969/j.issn.1671-654X.2014.05.018
JIANG Xiaowei, ZHU Shuhua, LI Guohong,et al. Research on layered extension of composite laminates with layered defects[J]. Aeronautical Computing Technology,2014,44(5):73-76(in Chinese). doi: 10.3969/j.issn.1671-654X.2014.05.018
|
[19] |
NILSSON K F, ASP L E, ALPMAN J E, et al. Delamination buckling and growth for delaminations at different depths in a slender composite panel[J]. International Journal of Solids & Structures, 2001, 38(17): 3039-3071.
|
[20] |
刘雅玲, 王康康, 赵丽滨. 含预制分层复合材料层合板的压缩失效行为研究[C]//北京力学会第二十三届学术年会会议论文集. 北京: 北京力学会, 2017: 2.
LIU Yaling, WANG Kangkang, ZHAO Libin. Study on compression failure behavior of laminated plates containing precast laminated composites[C]//Proceedings of the 23rd Annual Conference of Beijing Society of Mechanics. Beijing: Beijing Society of Mechanics, 2017: 2(in Chinese).
|
[21] |
RHEAD A T, BUTLER R, HUNT G W. Compressive strength of composite laminates with delamination-induced interaction of panel and sublaminate buckling modes[J]. Composite Structures, 2017, 171: 326-334.
|
[22] |
ASTM. Standard test method for tensile properties of polymer matrix composite materials: ASTM D3039/D3039M—17[S]. West Conshohocken: ASTM International, 2017.
|
[23] |
ASTM. Standard test method for compressive properties of polymer matrix composite materials using a combined loading compression (CLC) test fixture: ASTM D6641/D6641M—16[S]. West Conshohocken: ASTM International, 2016.
|
[24] |
ASTM. Standard test method for in-plane shear response of polymer matrix composite materials by tensile test of a ±45° laminate: ASTM D3518/D3518M—18[S]. West Conshohocken: ASTM International, 2018.
|
[25] |
ELICES M, GUINEA G V, GÓMEZ J, et al. The cohesive zone model: advantages, limitations and challenges[J]. Engineering Fracture Mechanics,2002,69(2):137-163. doi: 10.1016/S0013-7944(01)00083-2
|
[26] |
WANG R G, ZHANG L, ZHANG J, et al. Numerical analysis of delamination buckling and growth in slender laminated composite using cohesive element method[J]. Computational Materials Science, 2010, 50(1): 20-31.
|
[27] |
LIU P F, GU Z P, PENG X Q, et al. Finite element analysis of the influence of cohesive law parameters on the multiple delamination behaviors of composites under compression[J]. Composite Structures, 2015, 131: 975-986.
|
[28] |
TURON A, CAMANHO P P, COSTA J, et al. Accurate simulation of delamination growth under mixed-mode loading using cohesive elements: Definition of interlaminar strengths and elastic stiffness[J]. Composite Structures,2010,92(8):1857-1864. doi: 10.1016/j.compstruct.2010.01.012
|
[29] |
MOURA M F S F, GONÇALVES J P M, MARQUES A T, et al. Prediction of compressive strength of carbon-epoxy laminates containing delamination by using a mixed-mode damage model[J]. Composite Structures,2000,50(2):151-157. doi: 10.1016/S0263-8223(00)00091-X
|
[30] |
LAKSHMINARAYANA H V, BOUKHILI R, GAUVIN R. Impact response of laminated composite plates: Prediction and verification[J]. Composite Structures, 1994, 28(1): 61-72.
|
[31] |
HÜHNE C, ZERBST A K, KUHLMANN G, et al. Progressive damage analysis of composite bolted joints with liquid shim layers using constant and continuous degradation models[J]. Composite Structures,2010,92(2):189-200. doi: 10.1016/j.compstruct.2009.05.011
|
[32] |
张延林, 李秋阳. 碳布增强木质层合板的有限元渐进损伤分析[J]. 沈阳工业大学学报, 2017, 39(1):22-27.
ZHANG Yanlin, LI Qiuyang. Finite element progressive damage analysis of carbon fabric reinforced wood laminates[J]. Journal of Shenyang University of Technology,2017,39(1):22-27(in Chinese).
|
[33] |
LSTC. Keyword User’s Manual, Volume II[M]. Livermore: Version 11 R11.0. 0, 2018.
|
[34] |
HOU J P, PETRINIC N, RUIZ C, et al. Prediction of impact damage in composite plates[J]. Composites Science & Technology,2000,60(2):273-281.
|