[1] |
LI Xiaoyang, TAO Zhao, ZHANG Wei.
Reliability modelling for fatigue based on uncertain differential equation
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(8): 225820-225820.
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[2] |
WANG Qiuyi, WU Yanzeng, BAO Rui.
Analysis on CTOD corresponding parameters during fatigue crack growth
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(6): 526632-526632.
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[3] |
DUAN Jiatong, SUI Fucheng, LIU Hanhai, XIE Fang, OUYANG Tian, BAO Rui.
Fatigue crack growth performance of thin-walled structure under bending load
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(5): 524326-524326.
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[4] |
DUI Hongna, LIU Xiaodong, WANG Fan, DONG Jiang.
Crack growth model based on average growth rate
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2020, 41(11): 223887-223887.
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[5] |
GU Zhixu, ZHENG Jian, PENG Wei, ZHI Jianzhuang.
A viscoelastic damage constitutive model for HTPB with kinked growth of microcracks
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2018, 39(9): 222051-222059.
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[6] |
LI Zhenghong, XU Wu, ZHANG Xiaojing, YU Yin.
Experimental and analytical analyses of fatigue crack growth in sheets with multiple holes and cracks
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2018, 39(7): 221867-221867.
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[7] |
CHEN Jian, YUAN Shenfang, WANG Hui, QIU Lei.
Using Gaussian weighting-mixture proposal distribution particle filter for fatigue crack growth prediction
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2017, 38(11): 220925-220925.
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[8] |
ZHANG Xiaochen, XIE Liyang, ZHANG Ruijin, MENG Weiying, LI Ming, HU Jiexin.
‘Coaxing effect’of prior cycling stress on material fracture mechanics performance
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2016, 37(10): 3074-3082.
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[9] |
LIU Jianzhong;CHEN Bo;YE Xubin;HU Benrun;DING Chuanfu.
Fatigue and Crack Growth Behavior of Pre-corroded Aluminum Alloy 2024-T62 and Its Life Prediction Based on Fracture Mechanics
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2011, 32(1): 107-116.
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[10] |
Zhang Jikui;Li Zhengneng;Qiu Zhiping;Lei Jiafeng;Li Hongen;Yu Yang.
Feasibility Study on Damage Tolerance Design of Titanium Alloys
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2009, 30(4): 763-767.
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[11] |
Bian Guixue;Chen Yueliang;Zhang Danfeng;Yu Pinshi.
Study on Fatigue Life of Pre-corroded Aluminium Alloy Based on IDS
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2008, 30(6): 1526-1530.
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[12] |
WU Xue-ren;LIU Jian-zhong.
Total Fatigue Life Prediction for Aeronautical Materials by Using Small-Crack Theory
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2006, 27(2): 219-226.
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[13] |
ZHANG You-hong;LU Guo-zhi;CHEN Yue-liang;.
Predicting Fatigue Life From Pre-corroded LY12-CZ Aluminium Test
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2005, 26(6): 779-782.
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[14] |
TIAN Xiu-yun;SUN Zhi-qiang.
Curve Fitting Study on 2024-T42 Aluminium-Alloy Fatigue Crack G rowth
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2003, 24(2): 144-146.
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[15] |
GUO Wanlin;ZHANG Tianzhong .
EFFECTS OF THREE-DIMENSIONAL CONSTRAINT ON CRACK GROWTH UNDER AIRCRAFT SPECTRUM LOADING
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2000, 21(4): 294-298.
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