[1] |
Yunhe ZHAO, Shengnan WANG.
Solution to stress intensity factor by weight function method based on deep learning
[J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(19): 228367-228367.
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[2] |
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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[3] |
FENG Zhenyu, CHAI Chongbo, ZOU Jun, MOU Haolei.
Three-dimensional finite element analysis of stress intensity factors of butt-joints with multiple site damage
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(5): 524250-524250.
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[4] |
DENG Jian, LU Tianjian, YIN Qiaozhi.
Analysis on I-II mixed interlaminar crack propagation of composite MMB specimens
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(2): 224241-224241.
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[5] |
WANG Xueming, XIE Fuyuan.
Experimental study on behavior of delamination propagation of carbon fiber/bismaleimide composites during integral forming process
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(2): 424918-424918.
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[6] |
CAO Yuejie, WEI Lingfeng, ZHANG Minghao, CAO Zengqiang.
Experimental study on progressive failure mechanism of thin-laminate bolted joints
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(12): 424667-424667.
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[7] |
ZHAO Libin, GONG Yu, ZHANG Jianyu.
A survey on delamination growth behavior in fiber reinforced composite laminates
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2019, 40(1): 522509-522509.
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[8] |
ZHAO Xiaochen, WU Xueren, TONG Dihua, XU Wu, CHEN Bo, HU Benrun.
Accurate analytical weight function solutions for crack at edge of circular hole in infinite plate
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2018, 39(9): 221976-221987.
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[9] |
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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[10] |
LIU Shuangyan, LI Yulong, XUE Pu, SHI Xiaopeng.
Effect of crack parameters and stiffener layout on dynamic stress intensity factor of 3×3 grid stiffened panel at resonance
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2018, 39(1): 221423-221423.
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[11] |
CHAI Guozhong, LYU Jun, BAO Yumei, JIANG Xianfeng, DING Hao.
A highly efficient and accurate numerical analysis method for fatigue propagation of surface crack and life prediction
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2017, 38(12): 221291-221291.
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[12] |
SONG Danlong, ZHANG Kaifu, ZHONG Heng, LI Yuan.
Delamination damage and critical interference percentage for interference fit bolt joint of laminates
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2016, 37(5): 1677-1688.
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[13] |
ZHU Qingyu, HAN Feng, SUI Mingli.
Stress intensity factors and crack-surface opening displacements for two cracks emanating from a circular hole in an infinite plate
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2016, 37(3): 883-893.
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[14] |
TONG Dihua, WU Xueren, LIU Jianzhong.
Weight function method of determining double cantilever beam specimen stress intensity factor by crack mouth displacement
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2016, 37(2): 609-616.
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[15] |
WEI Yingying, AN Qinglong, CAI Xiaojiang, CHEN Ming.
CFRP ultrasonic scan delamination detection and evaluation method
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2016, 37(11): 3512-3519.
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