Chin J Mater Res  1992, Vol. 6 Issue (5): 450-454    DOI:

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FATIGUE CRACK GROWTH BEHAVIOR OF GLASS REINFORCE ALUMINUM LAMINATES

LIU Danmei;QU Wei;YANG Weifeng;ZHANG Reiping(Harbin Institute of Technology)XIA Yuebo(Institute of Metal Research;Academia Sinica)

LIU Danmei;QU Wei;YANG Weifeng;ZHANG Reiping(Harbin Institute of Technology)XIA Yuebo(Institute of Metal Research;Academia Sinica). FATIGUE CRACK GROWTH BEHAVIOR OF GLASS REINFORCE ALUMINUM LAMINATES. Chin J Mater Res, 1992, 6(5): 450-454.

Abstract References Related Articles Recommended Metrics Download:  PDF(1530KB)  Export:  BibTeX | EndNote (RIS)       Abstract  In this paper,fatigue crack growth behavior and the delamination phenome-non under different stress levels of a new kind of hybrid composite-glass fiber reinforce alumi-num laminates(GLALL)have been investigated.It is found that fatigue crack growth rate Key words:  laminate      fatigue crack growth      delamination      Received:  25 October 1992      Service E-mail this article Add to citation manager E-mail Alert RSS （） Articles by authors URL:  https://www.cjmr.org/EN/     OR     https://www.cjmr.org/EN/Y1992/V6/I5/450 1 Marissen R.Report A 86-35180,American Institute of Aeronautics and Astronautics(AIAA)Technical Information Service 2 Bucci R J et al.In Proc 33rd International SAMPE Symp.Exhibition,Society for the Advancement of Material and Process Engineering,California,USA,1988:1237 3 Marissen R.Engineering Fracture Mechanism,1984;19:261 4 郑瑞琪,90年代复合材料发展展望研讨会论文集,北京:中国复合材料学会,1990: 5 束德林.金属力学性能.北京:机械工业出版社,1987年11月 [1] WANG Yankun, WANG Yu, JI Wei, WANG Zhihui, PENG Xiangfei, HU Yuxiong, LIU Bin, XU Hong, BAI Peikang. Microstructure and Mechanical Properties of Carbon Fiber/Aluminum Laminated Composites[J]. 材料研究学报, 2022, 36(7): 536-544. [2] LIU Xiaoyan, LIU Kuijun, YANG Xirong, WANG Jingzhong, LUO Lei. Fatigue Crack Propagation Behavior of Ultrafine Grained Pure Titanium[J]. 材料研究学报, 2020, 34(6): 417-424. [3] CHEN Shaojie, XU Yanying, WANG Zhi, HU Po. Combustion Characteristics of Carbon Fiber/Epoxy Laminates at Low Heat Flux[J]. 材料研究学报, 2020, 34(12): 933-938. [4] Ruiyan GUO, Guoli ZHANG, Hailiang YUE, Huan MA, Lianyun CHEN. Evaluation of Compression after Impact on Composite Laminates Coated with PU[J]. 材料研究学报, 2017, 31(7): 526-536. [5] LIANG Enquan, HUANG Sensen, MA Yingjie, ZHANG Ren, LEI Jiafeng, LIU Yang. The Influence of Fe on the Mechanical Properties of Ti-6Al-4V ELI Alloy[J]. 材料研究学报, 2016, 30(4): 299-306. [6] Xiaojiao ZUO,Xiaoguang YUAN,Hongjun HUANG,Huan LIU. Effect of Heat Treatment on Microstructure of Interfacial Diffusion Layer of Cu/Al Composite Laminate Prepared by Cold Rolling[J]. 材料研究学报, 2014, 28(7): 528-534. [7] Zaoyu SHEN,Guanghong HUANG,Limin HE,Rende MU,Zhendong CHANG. Preparation and Thermal Stability of Large-sized TiAl/Ti3Al Micro-laminated Thin Sheets[J]. 材料研究学报, 2014, 28(4): 314-320. [8] ZHENG Sanlong CHEN Binbin ZHANG Wei GAO Zengliang**. An Experimental Study of Fatigue Crack Growth in Different Orientation of Extruded #br#AZ31B Mg Alloy Bar[J]. 材料研究学报, 2013, 27(4): 360-366. [9] SONG Peilong YANG Xuefeng WANG Shouren YANG Liying. Mechanical and Tribological Properties of Laminated Al2O3/TiC–Al2O3/TiC/CaF2 Self-lubrication Ceramic Material[J]. 材料研究学报, 2012, 26(5): 538-544. [10] WANG Rizhi; FENG Qingling; CUI Fuzhail LI Hengde(Tsinghua University). DEVELOPMENT OF BIOMIMETIC DESIGNED ALUMINA / FIBRE REINFORCED EPOXY LAMINATED COMPOSITE[J]. 材料研究学报, 1996, 10(1): 95-100. [11] LI Jianli;LI Xiaoming;XIE Genshuan; YAO Zhiming;LI Jin; KE Wei(National Laboratory of Corrosion and Protection.Institute of Corrosion and Protection ofmelals.Academia Sinica.Fushun Petroleum Institute)(Corresponent:LI Jianli;Mechanical Department;Fushun P. EFFECT OF HYDROGEN ATTACK TEMPERATURE ON FATIGUE CRACK BEHAVIOR FOR 20G AND 15CrMo STEELS[J]. 材料研究学报, 1995, 9(6): 496-500. [12] ZHANG Zhiqiang; SHANG Chengiia; ZHI Rentao (Hubei Automotive Industries Institute) (University of Science and Technology Beijing). FRACTURE MECHANISM OF THE LAMINATED COMPOSITE CERAMICS OF ALUMINA[J]. 材料研究学报, 1995, 9(5): 477-480. [13] ZHONG Weihong;CHEN Changqi;KOU Changhe(Beijing University of Aeronautics and Astronautics)ZHENG RuiQi;LI Hongyun;HU Hongjun(Beijing Institute of Aeronautical Materials). EFFECTS OF RESIDUAL STRESS AND ADHESIVE ON FATIGUE CRACK GROWTH OF ARALL[J]. 材料研究学报, 1995, 9(3): 273-278. [14] JIAO Chengge; HOU Shu'e; LI Chunyu; ZHANG Lushan (Institute of Aeronautical Materials; Beijing). FRACTURE TOUGHNESS AND FATIGUE CRACK GROWTH RATE OF 7075T73510 ALLOY[J]. 材料研究学报, 1994, 8(1): 35-40. [15] SUI Guoxin ZHOU Benlian ZHENG Zongguang ZHOU Chengti (Institute of Metal Research;Chinese Academy of Sciences)(International Centre for Materials Physics;Chinese Academy of Sciences)SHI Changxu (National Natural Science Foundation of China). VINYLON REINFORCED ALUMINIUM LAMINATES(VIRALL)——A KIND OF NEWLY DEVELOPED SUPERHYBRID COMPOSITES[J]. 材料研究学报, 1993, 7(4): 365-368. No Suggested Reading articles found! Viewed Full text Abstract Cited   Shared      Discussed