並列タイトル等Elastic Bucking Analysis of Corrugated Plates Under Uniform Compression
タイトル（掲載誌）航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory TR-604
一般注記The buckling behavior of corrugated plates under compressive loadings is presented. The corrugated plate is divided into curved strip elements and applied to the finite element method by using trigonometric functions and polynomial functions, corresponding to axial and circumferential directions respectively. Numerical results are presented for corrugated plates of infinite width and finite width. In the range of short panel, axial length is small compared with the dimensions of corrugation, and the shell-type buckling mode is dominant. Upon increasing the axial length, plate-type buckling takes place at a length greater than critical value. Design formulae to predict the minimum load of shell-type buckling, plate-type buckling load, and critical length are obtained based on the numerical results.
資料番号: NALTR0604000
レポート番号: NAL TR-604
一次資料へのリンクURLhttps://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=44859&item_no=1&attribute_id=31&file_no=1
連携機関・データベース国立情報学研究所 : 学術機関リポジトリデータベース（IRDB）（機関リポジトリ）
提供元機関・データベース宇宙航空研究開発機構 : 宇宙航空研究開発機構リポジトリ