Publications

Son, K.S., Yang, H.S. and Guedes Soares, C. (2013), “Accidents of foreign workers at construction sites in Korea”, Journal of Asian Architecture and Building Engineering, Vol. 12(2), pp. 197-203

Solutions to the problems of deformation of laminated cylindrical shells of finite dimensions must satisfy the prescribed boundary conditions, which introduce complexities, that are far more difficult to handle, primary among them being asymmetrically placed boundary conditions, e.g., clamped-free. Balaraman et al. [1] obtained closed-form solutions for internally pressurized asymmetrically laminated cylindrical shells of finite length, under the framework of the classical lamination theory (CLT) and Love-Timoshenko kinematic relations, but presented numerical results were for unsymmetric cross-ply shells only [1]. Admissible boundary conditions were derived by Chaudhuri et al. [2] for an arbitrarily laminated internally pressurized cylindrical shell of finite length, under the framework of Donnellfs, Love-Timoshenko's and Sandersf kinematic relations, and the CLT. Chaudhuri et al. [3] derived a closed-form solution for arbitrarily laminated cylindrical shells with both ends simply-supported, and subjected to uniform internal pressure, under the framework of the CLT and Love-Timoshenkofs kinematic relations. Abu-Arja and Chaudhuri [4, 5] and Chaudhuri and Abu-Arja [6] presented closed-form solutions of cross-ply and angle-ply cylindrical shells under internal pressure, based on the constant shear-angle theory (CST), also known as firstorder shear deformation theory (FSDT). In what follows, a hitherto unavailable closedform solution for an unsymmetric cross-ply cantilever cylindrical shell of finite length, under uniform internal pressure, using Love-Timoshenko's kinematic relations under the framework of classical lamination theory (CLT), is presented.

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