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Volume 32, Issue 3, 2002
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Effect of Substructure in Strengthened Layer on Fatigue Strength of Pure Titanium
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钛合金%疲劳%孪晶%残余应力
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[1]
Zhang Jianbin,Fun Ding,Ma Qin.
Effect of Substructure in Strengthened Layer on Fatigue Strength of Pure Titanium
[J].Aerospace Materials & Technology,2002,32(3):47-49,53.
[2]
ZHENG Zhiteng,DONG Shu,XU Danjun.
Effect of Pores on The Fatigue Properties of Gas Tungsten Arc Welded TA15 Titanium Alloy Joint
[J].Aerospace Materials & Technology,2014,44(5).
[3]
Yang Shengqun,Meng Qingwu,Geng Lin,Wu Lin,Chen Yanbin.
Wear Resistance of Thermal Spraying Nickel-Coated Graphite Layer on Titanium Alloy
[J].Aerospace Materials & Technology,2007,37(3):58-60.
[4]
Chao Min.
Effect of Different Anodizing Processes on the Fatigue Strength of Aluminum Parts
[J].Hongdu Science and Technology,2002(3):26-32.
[5]
Effect of Surface Treatment on Bond Joint Strength of TB8 Titanium Alloy and Composite Material
[J].Journal of Aeronautical Materials
[6]
JIN Lei,SU Bin.
Research on Low Cycle Fatigue Properties of TA15 Titanium Alloy
[J].Journal of Aeronautical Materials,2005,25(2):16-19.
[7]
Effect of Heat Treatment on Mechanical Properties of Commercial Pure Titanium Self-piecing Riveted Joints
[J].Journal of Aeronautical Materials
[8]
TIAN Xiu-yun,LIU Yong.
Influence of Interference-Fit Riveting on Fatigue Strength
[J].Journal of Civil Aviation University of China,2006,24(4):9-10,15.
[9]
CHEN Xu,CUI Hai-tao,TIAN Zeng,ZHANG Hong-jian,HE Yan-lei.
Effects of Laser Shock Peening on High-Temperature Fretting Fatigue Life of Titanium Alloy
[J].Journal of Propulsion Technology,2020,41(4):903-909.
[10]
Huo Wenhui.
Study on the Application of LGDFR Method in Landing Gear Fatigue Strength Analysis
[J].Civil Aircraft Design and Research,2015(1):47.
[11]
BEN Lin,XU Fu-ren,WANG Xin-hua,et al.
Research on the Effect of Friction between Teeth on the Tooth Root Bending Fatigue Strength by using EHL
[J].Aviation Precision Manufacturing Technology,2004,40(2):32-34.
[12]
CHEN Yunquan,CAO Zengqiang,QIN Longgang,CHEN Lili,YAN Li.
Research on Fatigue Experimental of Interference Fit Riveting of Titanium Alloy Structure
[J].Aeronautical Manufacturing Technology,2017(4).
[13]
LIN Yueguo,Macro GIGLIOTTI,Marie Christine LAFARIE-FRENOT,Jinbo BAI.
Thermo-electrical Coupling Effect on Tensile and Fatigue Strength of Composite Materials for Aeronautical Application
[J].Acta Aeronautica et Astronautica Sinica,2014,35(12):3315-3323.
[14]
Cavitation Erosion on Surface of Pure Titanium in Water Cavitation Jet
[J].Journal of Aeronautical Materials
[15]
Liu,Fenglei.
Improvement of Fatigue Strength of High Strength Aerospace Fastener by Using Rolling
[J].Aeronautical Manufacturing Technology,2005(6):97-99.
[16]
高福洋,郁炎,刘志颖,蒋鹏,郭宇凡.
Mechanism of Grain Refinement of Pure Titanium by Friction Stir Welding
[J].Journal of Aeronautical Materials,2016(6):29-34.
[17]
许洪明,张阿盈,吕春光,储建恒.
Experimental Investigation on Strength and Fatigue of Repaired Composite Structure
[J].Aeronautical Science and Technology,2012(6):48-50.
[18]
DU Feng-shan,YAN Liang,DAI Sheng-long,YANG Shou-jie.
Study on Fatigue Performance of High Strength Aluminum Alloy
[J].Journal of Aeronautical Materials,2009,29(1):96-100.
[19]
LIU Wen-lina and MU Zhi-taob.
Research on Fatigue Strength Reduction Factor to Helicopter Dynamic Components
[J].Journal of Naval Aeronautical Engineering Institute,2007,22(4):439-442.
[20]
XU Jian-xin,MING Ping-wei,WANG Xu-dong.
Fatigue Life Evaluation of Titanium Alloy Welding Specimens
[J].Journal of Civil Aviation University of China,2006,24(5):30-33.
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