机械工程 |
|
|
|
|
层合板分层失效数值模拟与参数识别 |
籍庆辉, 朱平, 卢家海 |
1. 上海汽车集团股份有限公司 前瞻技术研究部,上海 201804;
2. 上海交通大学 机械系统与振动国家重点实验室, 上海 200240;
3. 上海交通大学 上海市复杂薄板结构数字化制造重点实验室,上海 200240 |
|
Numerical simulation and parameter identification of delamination failure for laminate |
JI Qing-hui, ZHU Ping, LU Jia-hai |
1. Research and Advanced Technology, SAIC Motor Corporation Limited, Shanghai 201804, China;
2. State Key Laboratory of Mechanical System and Vibration, Shanghai Jiao Tong University, Shanghai 200240, China;
3. Shanghai Key Laboratory of Digital Manufacture for Thin-walled Structures, Shanghai Jiao Tong University, Shanghai 200240, China |
引用本文:
籍庆辉, 朱平, 卢家海. 层合板分层失效数值模拟与参数识别[J]. 浙江大学学报(工学版), 10.3785/j.issn.1008-973X.2017.05.015.
JI Qing-hui, ZHU Ping, LU Jia-hai. Numerical simulation and parameter identification of delamination failure for laminate. JOURNAL OF ZHEJIANG UNIVERSITY (ENGINEERING SCIENCE), 10.3785/j.issn.1008-973X.2017.05.015.
|
参考文献(References):
[1] YAO L, ALDERLIESTEN R C, ZHAO M, et al. Discussion on the use of the strain energy release rate for fatigue delamination characterization [J]. Composites Part A: Applied Science and Manufacturing, 2014, 66: 65-72.
[2] MURRI G B. Effect of data reduction and fiber-bridging on Mode Ⅰ delamination characterization of unidirectional composites [J]. Journal of Composites Materials, 2014, 48(19): 2413-2424.
[3] REEDER J R. An evaluation of mixed-mode delamination failure criteria [R]. 104210, Hampton: NASA,1992.
[4] BENZEGGAGH M L, KENANE M. Measurement of mixed-mode delamination fracture toughness of unidirectional glass/epoxy composites with mixedmode bending apparatus [J]. Composites Science and Technology, 1996, 56(4): 439-49.
[5] LIUY M, ZHANG C, XIANG Y B. A critical plane-based fracture criterion for mixed-mode delamination in composite materials [J].Composites Part B: Engineering, 2015, 82: 212-220.
[6] 范学领,孙秦.复合材料分层断裂判据及扩展准则研究[J].计算力学学报,2011,28(3): 479-482.
FAN Xueling, SUN Qin. Study on composites delamination initiation and propagation criterion [J]. Chinese Journal of Computational Mechanics, 2011,28(3):212-220.
[7] PEREIRA A B, MORAIS A B. Mixed-mode Ⅰ + Ⅲ interlaminar fracture of carbon/epoxy laminates [J]. Composites Part A: Applied Science and Manufacturing, 2009, 40: 518-523.
[8] KRUEGER R. The Virtual crack closure technique: history, approach and applications. [R]. NASA/CR-2002-21162,Hampton: NASA, 2002.
[9] ROSA M M, MANUEL M F. Failure criteria for mixed mode delamination in glass fibre epoxy composites [J]. Composite Structures, 2010, 92(9): 2292-2298.
[10] KRUEGER R. Application of benchmark examples to assess the single and mixed-mode static delamination propagation capabilities in ANSYS [R]. NASA/CR-2012-217588, Hampton: NASA, 2012.
[11] 肖涛,左正兴,刘栋,等.基于虚拟裂纹闭合法计算裂纹扩展的能量释放率[J].北京理工大学学报,2010,30(1): 37-41.
XIAO Tao, ZUO Zheng-xing, LIU Dong, et al. Computation of the crack propagation energy release rate based on the virtual crack closure technique [J].Transactions of Beijing Institute of Technology, 2010, 30(1): 37-41.
[12] MOSLEM S, ANASTASIOS P, THOMAS K. Mixed-mode quasi-static failure criteria for adhesivelybondedpultruded GFRP joints[J]. Composites: Part A: Applied Science and Manufacturing, 2014, 59: 45-56.
[13] FLOROS I S, TSERPES K I, LOBEL T. Mode-I, mode-Ⅱ and mixed-mode Ⅰ/Ⅱ fracture behavior of compositebonded joints: Experimental characterization and numericalsimulation [J]. Composites Part B: Engineering, 2015, 78: 459-468.
[14] BUI Q V. A modified Benzeggagh-Kenanefracture criterion for mixed-mode delamination [J]. Journal of Composite Materials, 2011, 45(4): 389-413.
[15] PIRONDI A, GIULIESE G, MORONI F, et al. Comparative study of cohesive zone and virtual crack closure techniques for threedimensional fatigue debonding [J]. The Journal of Adhesion, 2014, 90(5/6):457-481.
[16] ASTM D5528. Standard test method for mode Ⅰ interlaminar fracture toughness of unidirectional fiber reinforced polymer matrix composites [S]. American: ASTM, 2001.
[17] HB 7403.碳纤维复合材料层合板Ⅱ型断裂韧性GIIc测试方法[S].北京:中国航空工业集团公司,1996.
HB 7403. Mode Ⅱ interlaminar fracture toughness GIIc of CFRP laminates [S]. Beijing: AVIC, 1996.
[18] ASTM D6671. Standard test method for mixed mode Ⅰ-mode Ⅱ interlaminar fracture toughness of unidirectional fiber reinforced polymer matrix composites [S]. American: ASTM, 2001.
[19] PEREIRA A B, MORAIS A B. Mixed mode Ⅰ + Ⅱ interlaminar fracture of glass/epoxy multidirectional laminates-Part 2: Experiments [J].Composites Science and Technology, 2006, 66(13): 1896-1902. |
|
Viewed |
|
|
|
Full text
|
|
|
|
|
Abstract
|
|
|
|
|
Cited |
|
|
|
|
|
Shared |
|
|
|
|
|
Discussed |
|
|
|
|