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Institute of Automotive Engineering
School of Mechanical Engineering
Shanghai Jiao Tong University
Education:
2004-2008 Ph.D. Shanghai Jiao Tong University
2001-2004 M.S.Dalian Jiao Tong University
1993-1997 B.S. Tongji University
Professional Experience:
2012.1-now, Associate Researcher, Shanghai Jiao Tong University, Shanghai, China
2011.2-2011.12, Assistant Researcher, Shanghai Jiao Tong University, Shanghai, China
2008.8-2011.2, Postdoctor, Shanghai Jiao Tong University, Shanghai, China
1997.7-2001.8, Assistant Engineer, Qiqihar Rolling Stock Company, Qiqihar, China
Research Interests:
Formulation and analysis of problems in applied mechanics, solid and structural mechanics.
Specialization in the theory and applications of the composite materials and structures, plate and shell theories.
Selected Publications:
[1] Zhi-Min Li, Pizhong Qiao. Buckling and postbuckling behavior of shear deformable anisotropic laminated beams with initial geometric imperfections subjected to axial compression. Engineering Structures, Vol. 85, pp. 277-292, 2015.
[2] Zhi-Min Li, Pizhong Qiao. Buckling and postbuckling of anisotropic laminated cylindrical shells under combined external pressure and axial compression in thermal environments. Composite Structures, Vol. 119, pp. 709-726, 2015.
[3] Zhi-Min Li, Pizhong Qiao. Nonlinear vibration analysis of geodesically-stiffened laminated composite cylindrical shells in an elastic medium. Composite Structures, Vol. 111, pp. 473-487, 2014.
[4] Zhi-Min Li, Pizhong Qiao. On an exact bending curvature model for nonlinear free vibration analysis of shear deformable anisotropic laminated beams with initial loads resting on two-parameter elastic foundations. Composite Structures, Vol.108, pp. 243-258, 2014.
[5] Zhi-Min Li. Thermal postbuckling behavior of 3D braided beams with initial geometric imperfection under different type temperature distributions. Composite Structures, Vol.108, pp. 924-936, 2014.
[6] Zhi-Min Li, Xiang-Dong Chen, Hai-Dong Yu. Large-amplitude vibration analysis of shear deformable laminated composite cylindrical shells with initial imperfections in thermal environments. ASCE, Journal of Engineering Mechanics, Vol. 140, no.3, pp. 552-565, 2014.
[7] Zhi-Min Li, Xiang-Dong Chen, Hua Wang. Exact analysis of postbuckling behavior of anisotropic composite slender beams subjected to axial compression. ASCE, Journal of Aerospace Engineering, Vol. 27, no. 2, pp. 318-324, 2014
[9] Jia Lin, Sun Jin, Cheng Zheng, Zhimin Li, Yinhua Liu. Compliant assembly variation analysis of aeronautical panels using unified substructures with consideration of identical parts. Computer-Aided Design, Vol.57, pp.29-40, 2014.
[10] Guo-Ping Chu, Zhi-Min Li. Postbuckling behavior of 3D braided rectangular plates subjected to uniaxial compression and transverse loads in thermal environments. Science China: Technological Sciences, Vol. 57, no. 7, pp. 1439-1457, 2014.
[11] Zhi-Min Li, Yi-Xi Zhao, Xiang-Dong Chen. Non-linear buckling and postbuckling behavior of 3D braided cylindrical panels under axial compression in thermal environments. Mechanics of Advanced Materials and Structures, Vol. 21, no. 6, pp. 490-504, 2014.
[12] Zhi-Min Li, Zhong-Qin Lin. Thermal postbuckling of shear-deformable anisotropic laminated cylindrical shells with temperature-dependent properties. International Journal of Non-Linear Mechanics, Vol.47, pp. 984-998, 2012.
[13] Zhi-Min Li, Wei Gu and Yi-Xi Zhao. Postbuckling behavior of 3D braided rectangular plates subjected to biaxial compression. ASCE, Journal of Aerospace Engineering, Vol. 25, no.4, pp. 680-690, 2012.
For more see the link:
Prof. Zhi-Min Li
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