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STRESS INTENSITY FACTOR OF DISSIMILAR ORTHOTROPIC LAMINATE WITH AN EDGE CRACK ALONG THE INTERFACE UNDER ANTI-PLANE LOADING
Zhang Xing, Chen Yige
1989, 6(2): 1-8,14.
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NONLINEAR BIMQDULUS MODEL AND STRENGTH OF 3D CARBON CARBON MATERIAL
Gu Zhenlong, Gao Qunyao, Zhang Weibo
1989, 6(2): 9-Ⅱ.
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A REFINED THEORY OF ORTHOTROPIC LAMINATED DOUBLY CURVED SHELL
Cai Siwei, Cai Min
1989, 6(2): 15-Ⅲ.
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AN ANALYSIS OF NON-LINEAR FLEXURAL FORCED VIBRATION OF ANISOTROPIC UNSYMMETRICALLY ANGLE-PLY LAMINATED PLATES
Li Hua, Shen Darong
1989, 6(2): 24-Ⅲ.
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BUCKLING ANALYSIS OF LAMINATED COMPOSITE CYLINDRICAL SHELLS WITH LONGITUDINAL RIBS
Wen Lizhou
1989, 6(2): 31-Ⅳ.
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POSTBUCKL1NG BEHAVIOUR OF ORTHOTROPIC RECTANGULAR PLATES
Wang Hu, Ou Maocai, Tsunkuei Wang
1989, 6(2): 39-Ⅴ.
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PROBABILISTIC PREDICTION OF LAMINATES WITH OR WITHOUT DELAMINATION
Wen Baicheng, Gu Zhenlong
1989, 6(2): 48-Ⅵ.
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FREE VIBRATIONS OF COMPOSTE LAMINATED BEAMS ON ELASTIC FOUNDATIONS
Deng Liangbo
1989, 6(2): 55-Ⅵ.
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STUDIES ON THE STRUCTURE AND PROPERTIES OF THE PITCH-BASED CARBON FIBER AND ITS HYBRID FIBER REINFORCED NYLON-1010 COMPOSITES
Zeng Hanmin, Kong Bailing, Chen Hongxiao
1989, 6(2): 61-Ⅶ.
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THE TWO ELEMENT-BIREFRINGENT PHENOMENA OF FIBRE-REINEFORCED COMPOSITES
Zhang Wu, Lin Wei, Luo Jian
1989, 6(2): 68-Ⅶ.
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OPTIMUM DESIGN OF COMPOSITE STRUCTURES SUBJECTED TO STATIC AND DYNAMIC CONSTRAINST
Xia Renwei, Wang Liping
1989, 6(2): 74-Ⅷ.
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OPTIMUM DESIGN OF COMPOSITE WING STRUCTURES SUBJECTED TO DISPLACEMENT CONSTRAINTS
Huang Chuanqi, Qiao Xin
1989, 6(2): 84-89.
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