[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] |
WAN Aoshuang.
Probabilistic assessment on damage tolerance of composite helicopter horizontal tail structure
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(6): 525557-525557.
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[3] |
WANG Houbing, WANG Xiahan, LIN Guowei, LI Xinxiang, YANG Shengchun.
Residual strength evaluation of curved hat-stiffened composite panels with discrete-source damage
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(6): 525899-525899.
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[4] |
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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[5] |
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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[6] |
LIU Zongxing, LIU Jun, LI Weina.
Dynamic response and failure of typical fuselage structure under blast impact load
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(2): 224252-224252.
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[7] |
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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[8] |
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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[9] |
DONG Anqi, ZHAO Xinqing, ZHAO Yan.
Tension-tension fatigue performance of unidirectional out-of-autoclave composite manufactured by automated fiber placement
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2018, 39(2): 421422-421422.
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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] |
CHEN An, WEI Yulong, LIAO Jianghai, DONG Dengke, WANG Xu.
Damage tolerance test of stiffened fuselage panel under complex load
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2017, 38(1): 420093-420093.
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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] |
HAO Yanguang, LIU Jianzhong, GUO Xiang, LIU Hu, SHANG Deguang.
Residual strength prediction of welded stiffened thin-walled structures made of Al 6156-T4 alloy based on CTOD method
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2015, 36(3): 827-833.
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