Closed-Form Solution of Thin and Moderately Thick Anisotropic Cylinders under Torsion, Axial Compression and Combined Load

Author:

TAKANO Atsushi

Publisher

Japan Society for Aeronautical and Space Sciences

Reference11 articles.

1. 3) Hyer, M. W. and Paraska, P. J.: Innovative Design of Composite Structures: Axisymmetric Deformations of Unsymmetrically Laminated Cylinders Loaded in Axial Compression, Dept. of Engineering Science and Mechanics, VPI-E-90-10 Report, VA Tech, 1990.

2. 4) Nemeth, M. P. and Smeltzer, III.S.S.: Bending Boundary Layers in Laminated-Composite Circular Cylindrical Shells, NASA TP-2000-210549, 2000.

3. 5) Nemeth, M. P. and Schultz, M. R.: The Exact Solution for Linear Thermoelastic Axisymmetric Deformations of Generally Laminated Circular Cylindrical Shells, NASA TP-2012-217342, 2012.

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