並列タイトル等BUCKING OF CYLINDRICAL SHELLS WITH CIRCULAR CUTOUTS UNDER AXIAL 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-560
一般注記An experimental and analytical study was proceeded to examine the effects of circular cutouts on the bucking behavior of cylindrical shells under axial compression. The experimental results were obtained from tests performed on polyester, brass, and aluminum shells with two diametrically opposed circular and were compared with available experimental data for shells with a single circular cutout. A Rayleigh-Ritz approximation was used to derive close-form solution which shows the governing parameter of the problem explicitly.
資料番号: NALTR0560000
レポート番号: NAL TR-560
一次資料へのリンクURLhttps://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=44814&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