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Dept. of Aeronautics and Astronautics, National Cheng Kung University, Tainan, Taiwan
Selected Publications:
L.-C. Shiau and J.-T. Chang, “Transverse shear effect on vibration of laminated plate using higher-order plate element,” Computers & Structures, vol. 39, no. 6, pp. 735–740, 1991.
Shiau L.C., Lu L.T.: Nonlinear flutter of two-dimensional simply supported symmetric composite laminated plates. J. Aircr. 29, 140–145 (1992)
L.C. Shiau, “Flutter of composite laminated beam plates with delamination”, AIAA J, 30 (10) (1992), pp. 513-523
Shiau L.C., Wu T.Y.: A high precision higher order triangular element for free vibration of general laminated plates. J. Sound vib. 161, 265–279 (1993)
Shiau Le-Chung (Institute of Aeronautics and Astronautics, National Cheng Kung University, Tainan, Taiwan, R.O.C.), “A finite element procedure for inelastic dynamic analysis of cylindrical structures”, Computers & Structures, Vol. 48, No. 3, August 1993, pp. 481-486
Wu, T., Shiau, L., 1995, Application of the Finite Element Method to Postbuckling Analysis of Laminated Plates, AIAA Journal, VoI. 33, No. 12, pp. 2379-2385.
Shiau, L.C. and Kuo, S.Y. (2004), “Thermal buckling of composite sandwich plates”, Mech. Based Design Struct. Machines, 32(1), 57-72.
L. C. Shiau and S. Y. Kuo, “Thermal postbuckling behavior of composite sandwich plates”, J. Eng. Mech. ASCE 130:10 (2004), 1160–1167.
L.C. Shiau, S.Y. Kuo, Free vibration of thermally buckled composite sandwich plates, ASME J Vib Acoust, 128 (1) (2006), pp. 1–7
Shih-Yao Kuo, Le-Chung Shiau and Ke-Han Chen, “Buckling analysis of shape memory alloy reinforced composite laminates”, Composite Structures, Vol. 90, No.2, September 2009, pp. 188-195
Yao S., Kuo., Le-Chung Shiau., 2009, Buckling and vibration of composite laminated plates with variable fiber spacing, Composite Structures 90(2): 196-200.
L. C. Shiau, S. Y. Kuo and C. Y. Chen, Thermal buckling behavior of composite laminated plates, Compos. Struct. 92 (2010) 508–514.
L.-C. Shiau, S.-Y. Kuo and S.-Y. Chang, Free vibration of buckled SMA reinforced composite laminates, Compos. Struct. 93 (11) (2011) 2678–2684.
S.-Y. Kuo, L.-C. Shiau, and C.-H. Lai, “Flutter of buckled shape memory alloy reinforced laminates,” Smart Materials and Structures, vol. 21, no. 3, Article ID 035020, 2012.
Shiau, L.C., Kuo, S.Y. and Liu, Y.P. (2012), “Aerothermoelastic analysis of composite laminated plates”, Compos. Struct., 94, 1982-1990.
Shih-Yao Kuo, Le-Chung Shiau, Jing-Wei Chuang and Chien-Chin Cheng, “The relationship of buckle pattern change and vibration mode shifting: Thermal postbuckling and vibration of composite laminates”, Journal of Aeronautics, Astronautics and Aviation, Vol. 48, No. 1, pp 65-74, 2016
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