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• DISLOCATION EMISSION AND EQUATION OFENERGY BARRIERS AT MODEL I CRACK TIP

  来源： 《中国有色金属学报(英文版)1996年第1期》——Zou Hongcheng Dai Shujuan Liu Furong Hu Xiangyang Li Changchun

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• Fracture toughness and fatigue crack growth analysis of 7050-T7451 alloy thick plate with different thicknesses

  来源： 《中南大学学报(英文版)2014年第8期》——WANG Yi-lin(王艺淋) PAN Qing-lin(潘清林) WEI Li-li(韦莉莉) LI Bo(李波) WANG Ying(王迎)

  Fracture toughness and fatigue crack growth analysis of 7050-T7451 alloy thick plate with different thicknessesWANG Yi-lin(王艺淋)1, PAN Qing-lin(潘清林)1, 2, WEI Li-li(韦莉莉)1, LI Bo(李波)1, WANG Ying(王迎)1(1... University), Changsha 410083, China)Abstract:The strength, fracture toughness and fatigue crack growth resistance of 7050-T7451 aluminum alloy plate with different thicknesses (35 mm and 160 mm) were......

• GH4742合金疲劳裂纹扩展行为

  来源： 《中国有色金属学报2017年第9期》——张宝宁 袁超 郭建亭 秦鹤勇 赵光普

  ) 图11  裂纹遇到晶界扩展进入下一个晶粒时发生偏转和扭转的模型图[20] Fig. 11  Shematic illustration of deflection and twist of crack propagating into adjacent grain[20] 3  结论 1) 随着温度的升高,GH4742合金的裂纹扩展寿命降低,裂纹扩展速率增加.在低... dimensions for fatigue crack growth (FCG) test (Unit: mm) 实验分别在室温,700 ℃及750 ℃ 3个温度进行,为保证数据的可靠性,每个温度下测试3个样品.疲劳裂纹扩展实验在MTS810型疲劳机上完成,控制方法采用的是恒力幅测定材料的疲劳裂纹扩展速率da/dN,波形为正弦波,加载频率为10 Hz,应力比为0.1.本实验中采集的数据是裂纹扩展......

• A CRACK CLOSURE MODEL FOR BRITTLE ROCK SUBJECTED TO COMPRESSIVE-SHEAR LOADING

  来源： 《中国有色金属学报(英文版)1999年第2期》——Chen Feng Sun Zongqi Xu Jicheng

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• Crack Initiation under Cyclic Compression

  来源： 《JOURNAL OF MATERIALS SCIENCE TECHNOLOG1989年第5期》——冯美斌 陈新增 何家文

  Crack Initiation under Cyclic Compression冯美斌,陈新增,何家文摘 要:<正> The crack initiation behaviour under cycliccompression foy the notched specimen wasinvestigated. It has been found that the cyclesfor crack initiation increase with the increaseof compressive mean stress, and the decreaseof stress amplitude. The stress amplitude playsa more important role......

• Effect of pre-strain on fatigue crack growth of 2E12 aluminum alloy

  来源： 《中国有色金属学报(英文版)2007年增刊第1期》——易丹青 杨胜 邓斌 周明哲

  Effect of pre-strain on fatigue crack growth of 2E12 aluminum alloy YI Dan-qing(易丹青)1, 2, YANG Sheng(杨胜)1, 2, DENG Bin(邓斌)1, ZHOU Ming-zhe(周明哲)1 1. School of Materials Science and Engineering...> Abstract: The influences of pre-strain on the mechanical property and fatigue crack growth of 2E12 aluminum alloy were evaluated by SEM, TEM, mechanical property and fatigue tests......

• Simulating weld hot crack of T-type joints of aluminum plates with ANN

  来源： 《中国有色金属学报(英文版)2005年第z2期》——董志波 魏艳红 B. Yakushin D. Semin

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• Microstructure and crack sensitivity of electron beam welded titanium aluminide joints

  来源： 《中国有色金属学报(英文版)2005年第z2期》——吴会强 冯吉才 何鹏 何景山

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• 热应力作用下碳化钨基钢结硬质合金梯形裂纹的形成机理

  来源： 《中国有色金属学报2003年第5期》——尤显卿 郑玉春 程娟文 任昊

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• 基于扩展有限元法的齿根裂纹扩展规律

  来源： 《中南大学学报(自然科学版)2016年第8期》——唐进元 许德涛 周炜

  propagating toward tooth circumferential direction until fracture happens for the model used. Compared to position of initial crack, length and direction have less influence on crack propagation path...:1672-7207(2016)08-2668-08 Tooth root crack propagation regularity based on extended finite element method XU Detao, TANG Jinyuan, ZHOU Wei (Key Laboratory of Modern Complex Equipment Design......