General Higher-Order Theory of Laminated Composite Structures Assuming Displacements in Each Layer

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概要

• 論文の詳細を見る

• A general higher-order approximation theory to analyze static and/or dynamic behaviors of laminated composite structures is established. Theoretical characteristics and validity of the theory are made clear by numerical examples. The theory is formulated by using a modified Hamilton's principle for relaxed displacement continuity requirement, after expanding displacements of each lamina using power series in the thickness direction. The independent unknown variables of this theory are displacement coefficients of each lamina and interlaminar stresses. It is shown that the present theory takes account of the previous theories, and improves the inconsistencies of those theories.

• 一般社団法人日本機械学会の論文
• 1994-07-15

著者

• Hirashima K

  Yamanashi Univ. Kofu Jpn

• Hirashima Ken-ichi

  Department Of Civil Engineering Yamanashi University

• NEGISHI Yoshikazu

  Department of Civil Engineering, Fukushima National College of Technology

• Negishi Y

  Fukushima National Coll. Technol. Iwaki Jpn

• Negishi Yoshikazu

  Department Of Civil Engineering Fukushima National College Of Technology

関連論文

• Stress Distributions around Circular Inclusion in Infinite Plane for Nonlocal Elasticity : Matrix and Circular Inclusion have the Same Nonlocal Coefficients
• General Higher-Order Theory for Laminated Composite Structures with Interlayer Slip
• General Higher-Order Theory of Laminated Composite Structures Assuming Displacements in Each Layer

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