| [1] |
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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| [2] |
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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| [3] |
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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| [4] |
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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| [5] |
ZHAO Tian, YANG Zhichun, TIAN Wei, CHEN Zhaolin.
Vibration and acoustic radiation characteristics analysis of composite laminated plate in hygrothermal environments
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2017, 38(10): 221038-221038.
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| [6] |
DENG Jian, ZHOU Guangming, YIN Qiaozhi, XIANG Chao, CAI Deng'an.
Progressive damage analysis of double-strap bonding repaired laminates under buckling compression
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2016, 37(5): 1526-1535.
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| [7] |
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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| [8] |
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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| [9] |
ZHOU Zhenggan, SUN Guangkai, CHEN Xiucheng, WANG Jie.
Quantitative Characterization Test of Fastening Hole Delamination in Composites with Laser Ultrasonics
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2014, 35(8): 2348-2354.
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| [10] |
GAO Shangjun, YU Zhefeng, WANG Hai.
Prediction of Delamination Threshold Load for Impact on Composite Laminate Based on Modified Interlaminar Shear Strength Criterion
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2014, 35(5): 1329-1335.
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| [11] |
YUAN Jianfeng, NI Zao, CHEN Baoxing.
Buckling of SSCC Composite Laminates Under In-plane Bending Load
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2014, 35(4): 1026-1033.
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| [12] |
LI Biao, LI Yazhi, HU Bohai.
A New Interfacial Element and Finite Element Model for Composite Laminates
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2013, 34(6): 1370-1378.
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| [13] |
Cheng Xiaoquan;Zou Jian;Zhang Jikui;Li Zhengneng.
Properties of Stitched Composite Laminates—Fatigue Performance of Composite Laminates with an Open-hole
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2009, 30(5): 867-871.
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| [14] |
Wang Xueming;Xie Fuyuan;Li Min;Dai Di;Wang Fei;Zhang Zuoguang.
Effect Rules of Complex Structure on Manufacturing Defects for Composites in Autoclave Molding
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2009, 30(4): 757-762.
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| [15] |
Qi Lei;Li Min;Gu Yizhuo;Sun Zhijie;Zhang Zuoguang.
Experimental Study on Hygrothermal Properties of Several Kinds ofCarbon Fiber/BMI Resin Composites
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2009, 30(12): 2476-2480.
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