DESIGN OPTIMIZATION FOR STRUCTURAL THERMAL BUCKLING
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Biaosong Chen | Yuanxian Gu | Guozhong Zhao | Guozhong Zhao | Biaosong Chen | J. Kuang | Tse-Yung P. Chang | Wei Lin | Tse-Yung Paul Chang | Jun S. Kuang | Yuanxian Gu | Wei Lin
[1] John Argyris,et al. Recent Advances in Computational Thermostructural Analysis of Composite Plates and Shells With Strong Nonlinearities , 1997 .
[2] Georg Thierauf,et al. Thermal buckling optimization of composite laminates by evolution strategies , 2000 .
[3] Ahmed K. Noor,et al. Computational Models for High-Temperature Multilayered Composite Plates and Shells , 1992 .
[4] Gengdong Cheng,et al. Structural modelling and sensitivity analysis of shape optimization , 1993 .
[5] Niels Olhoff,et al. Optimization of the buckling load for composite structures taking thermal effects into account , 2001 .
[6] R. Haftka,et al. Design for temperature and thermal buckling constraints employing a noneigenvalue formulation , 1983 .
[7] Ahmed K. Noor,et al. Thermomechanical buckling and postbuckling of multilayered composite panels , 1993 .
[8] M. Autio,et al. Optimization of coupled thermal-structural problems of laminated plates with lamination parameters , 2001 .
[9] T. R. Tauchert,et al. Thermally Induced Flexure, Buckling, and Vibration of Plates , 1991 .
[10] Earl A. Thornton,et al. Thermal Buckling of Plates and Shells , 1993 .
[11] Earl A. Thornton,et al. Thermal Structures for Aerospace Applications , 1996 .
[12] Raimund Rolfes,et al. High Performance 3D-Analysis of Thermo-Mechanically Loaded Composite Structures , 1999 .
[13] A. R. de Faria,et al. Optimal buckling loads of nonuniform composite plates with thermal residual stresses , 1999 .
[14] Raphael T. Haftka,et al. Techniques for thermal sensitivity analysis , 1981 .
[15] A. Noor,et al. Thermomechanical Buckling of Multilayered Composite Plates , 1992 .
[16] Raphael T. Haftka,et al. Recent developments in structural sensitivity analysis , 1989 .
[17] R. Haftka,et al. Sensitivity Analysis of Discrete Structural Systems , 1986 .