[1] |
CHEN Yong, LIAO Gaojian, REN Lihai, LIU Xi.
Damage tolerance of GLARE laminates subjected to high-velocity impact
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2018, 39(7): 221733-221733.
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[2] |
OUYANG Xiaosui, LIU Yi.
Panel flutter of variable stiffness composite laminates in supersonic flow
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2018, 39(3): 221539-221539.
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[3] |
MENG Weiying, XIE Liyang, LIU Jianzhong, BAI Xin, TONG Anshi.
Contrast study on fatigue life performance of glass fiber reinforced Al-Li alloy laminates under unimodal overload
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2016, 37(5): 1536-1543.
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[4] |
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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[5] |
REN Shangkun, XU Zhenhan.
Evaluating of Microstructure Damage and Strain for Ferromagnetic Specimens Based on Sensitive Differential Susceptibility
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2014, 35(5): 1452-1458.
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[6] |
ZHANG Xiangyang, LI Yong, CHU Qiyi, XIAO Jun, DONG Xiaoyang.
Influence of Z-pins Insertion Pattern on In-plane Compression Properties of Laminates
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2014, 35(1): 195-202.
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[7] |
ZHOU Pei, REN Jilin, SUN Jinli, SONG Kai, WANG Zhen.
Application of Lissajous Figure in Two-dimensional Magnetic Memory Detection
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2013, 34(8): 1990-1997.
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[8] |
JIANG Jiefeng, DONG Huiyue, BI Yunbo.
Analysis of Process Parameters Influencing Protuberance During Interference Fit Installation of Hi-lock Bolts
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2013, 34(4): 936-945.
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[9] |
REN Jilin, CHEN Xi, LUO Shengcai, ZHOU Pei, LIU Changkui.
Research of High-cycle Fatigue Damage by Two-dimensional Magnetic Memory Testing
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2012, (6): 1147-1155.
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[10] |
Chen Yuanfang;Li Yulong;Liu Jun;Liu Yuanyong.
Study of Bird Strike on an Improved Leading Edge Structure
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2010, 31(9): 1781-1787.
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[11] |
Zheng Xiaoxia;Zheng Xitao;Shen Zhen;Yang Shengchun.
Damage Equivalent of Composite Laminates Subjected to Drop-weight Impact and Quasi-static Indentation Force
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2010, 31(5): 928-933.
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[12] |
Liu Changkui;Tao Chunhu;Chen Xing;Dong Shiyun.
Fatigue Damage Model of Notched 18CrNi4A Steel Specimens by Metal Magnetic Memory Method
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2009, 30(9): 1641-1647.
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[13] |
Lian Wei;Yao Weixing.
Strength Predicting Method of Composite Laminates with a Central Hole Based on FEA Simulation
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2009, 30(8): 1440-1446.
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[14] |
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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[15] |
Lian Wei;Yang Zhongqing;Yao Weixing.
Method of Estimating In-plane Shear S-N Curve of Unidirectional Laminate from Off axis Tension S-N Curve
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2009, 30(4): 637-642.
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