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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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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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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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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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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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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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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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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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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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HU Weiping;MENG Qingchun;ZHANG Xing .
METHOD OF STATE DECOMPOSITION AND TRIGONOMETRIC SERIES ON ELLIPTICAL DELAMINATION IN COMPOSITE LAMINATE
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2000, 21(4): 338-342.
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ZHANG Yan hui;LI Wei ji .
MULTIOBJECTIVE OPTIMUM DESIGN APPROACH BASED ON FUZZY IMPORTANCE
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1999, 20(4): 68-70.
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Shu Xiaoping .
REFINED DELAMINATION MODEL FOR LAMINATED BEAMS
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1998, 19(2): 236-239.
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Zhang Kaida.
FATIGUE DAMAGE CUMULATION AND LIFE PREDICTION FOR CARBON/BISMALEIMIDE COMPOSITE LAMINATES
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1997, 18(5): 623-624.
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Qian Chun;Yang Jialing;Xi Feng.
NONLINEAR DYNAMIC STABILITY OF COMPOSITE LAMINATED CYLINDRICAL PANELS
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1996, 17(S1): 95-98.
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Zhong Weihong;Chen Changqi;Kou Changhe;Zheng Ruiqi.
EXPERIMENTAL STUDY ON EFFECTS ON DELAMINATION NEAR CRACK OF ARALL BY RESIDUAL STRESS UNDER FATIGUE AND STATIC LOADS
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1996, 17(2): 196-201.
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CJA
