ANALYSIS OF THE MECHANICAL BEHAVIOR OF FIBER-REINFORCED COMPOSITES IN THE POST-FAILURE STATE.

Hiroichi Ohira; Nobuhide Uda

ANALYSIS OF THE MECHANICAL BEHAVIOR OF FIBER-REINFORCED COMPOSITES IN THE POST-FAILURE STATE.

Hiroichi Ohira
, Nobuhide Uda

航空宇宙機構造強度

研究成果: 書籍/レポートタイプへの寄稿 › 会議への寄与

抄録

A theory is presented which predicts the post-failure behavior of laminated plates subjected to combined inplane loads. To take account of the post-failure state, two idealized material properties are assumed, i. e. , the ductile matrix and the brittle matrix. Throughout the process from the initial failure to the final fracture, the detailed behavior of the laminate can be analyzed. A method for analyzing the unloading and reloading behavior is also given.

本文言語	英語
ホスト出版物のタイトル	Theoretical and Applied Mechanics
出版社	Univ of Tokyo Press
ページ	137-145
ページ数	9
ISBN（印刷版）	4130660926
出版ステータス	出版済み - 1985

出版物シリーズ

名前	Theoretical and Applied Mechanics
巻	33
ISSN（印刷版）	0285-6042

!!!All Science Journal Classification (ASJC) codes

材料力学

他のファイルとリンク

引用スタイル

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title = "ANALYSIS OF THE MECHANICAL BEHAVIOR OF FIBER-REINFORCED COMPOSITES IN THE POST-FAILURE STATE.",

abstract = "A theory is presented which predicts the post-failure behavior of laminated plates subjected to combined inplane loads. To take account of the post-failure state, two idealized material properties are assumed, i. e. , the ductile matrix and the brittle matrix. Throughout the process from the initial failure to the final fracture, the detailed behavior of the laminate can be analyzed. A method for analyzing the unloading and reloading behavior is also given.",

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N2 - A theory is presented which predicts the post-failure behavior of laminated plates subjected to combined inplane loads. To take account of the post-failure state, two idealized material properties are assumed, i. e. , the ductile matrix and the brittle matrix. Throughout the process from the initial failure to the final fracture, the detailed behavior of the laminate can be analyzed. A method for analyzing the unloading and reloading behavior is also given.

AB - A theory is presented which predicts the post-failure behavior of laminated plates subjected to combined inplane loads. To take account of the post-failure state, two idealized material properties are assumed, i. e. , the ductile matrix and the brittle matrix. Throughout the process from the initial failure to the final fracture, the detailed behavior of the laminate can be analyzed. A method for analyzing the unloading and reloading behavior is also given.

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UR - https://www.scopus.com/pages/publications/0022269847#tab=citedBy

M3 - Conference contribution

AN - SCOPUS:0022269847

SN - 4130660926

T3 - Theoretical and Applied Mechanics

SP - 137

EP - 145

BT - Theoretical and Applied Mechanics

PB - Univ of Tokyo Press

ER -

ANALYSIS OF THE MECHANICAL BEHAVIOR OF FIBER-REINFORCED COMPOSITES IN THE POST-FAILURE STATE.

抄録

出版物シリーズ

!!!All Science Journal Classification (ASJC) codes

他のファイルとリンク

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