An Exact Exponential Theory for the Bending of Simply Supported Laminated Orthotropic Plates (Solid Mechanics and Material Engineering)

スポンサーリンク

概要

• 論文の詳細を見る

• A laminated orthotropic plate theory is developed on the assumption that inplane displacements vary exponentially across plate thickness. Analytical solutions are obtained for simply supported, symmetric and anti-symmetric cross-ply rectangular laminates under transverse loading. The numerical results are compared with solutions of the three-dimensional elasticity theory, the third-order shear deformation theory, and the first-order shear deformation theory. It is found that the present exact exponential theory provides very accurate displacements and stresses in comparison to the three-dimensional elasticity theory. In particular, both transverse shear from constitutive equations and transverse normal stresses from equilibrium equations are more accurate than previously developed theories, even for small length-to-thickness ratios.

• 社団法人日本機械学会の論文
• 2003-04-15

著者

• Park J

  Hankuk Aviation Univ. Kyonggi Kor

• Park J

  Kosha Inchon Kor

• Park Jungsun

  School Of Aerospace And Mechanical Engineering Hankuk Aviation University

• LEE Soo-Yong

  School of Aerospace and Mechanical Engineering, Hankuk Aviation University

• Lee S‐y

  Hankuk Aviation Univ. Kyonggi Kor

• Lee Soo-yong

  School Of Aerospace And Mechanical Engineering Hankuk Aviation University

関連論文

• DISCRETE OPTIMAL DESIGN OF COMPOSITE SATELLITE COMPONENTS
• Epidemiological Characteristics of Workers' Sudden Death as Claims Due to Work Stress
• A New Exponential Plate Theory for Laminated Composites under Cylindrical Bending
• An Exact Exponential Theory for the Bending of Simply Supported Laminated Orthotropic Plates (Solid Mechanics and Material Engineering)

スポンサーリンク