[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] |
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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[6] |
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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[7] |
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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[8] |
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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[9] |
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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[10] |
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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[11] |
SUN Xian-nian;ZHENG Chang-liang.
Advances on Modeling Through-the-thickness Reinforcement of Laminated Composite by z-pinning
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2006, 27(6): 1194-1202.
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[12] |
ZHANG Shuang;WANG Dong;LI Zheng-neng;KOU Chang-he;ZHANG Yi-ning.
Parameterized Simulation for Composite Laminates with Single Mechanically Fastened Joint Based on ANSYS
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2006, 27(6): 1088-1091.
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[13] |
YAN Ying;ZENG Dong.
Study on the Post-Impact Compressive Strength of Composite Lamin ates
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2003, 24(2): 137-139.
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[14] |
GUI Liang jin;CHENG Xiao quan;KOU Chang he;LI Zheng neng;XIE Xiang li.
EFFECTS OF STITCHING ON STRENGTH AND IMPACT DAMAGE RESISTANCE OF COMPOSITE LAMINATES
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2000, 21(4): 368-371.
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[15] |
HU Zili.
COMPRESSIVE BUCKLING FAILURE OF LAMINATES WITH A SURFACE NOTCH
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2000, 21(1): 25-29.
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