並列タイトル等Vibration and Buckling Analysis of Ring-Stiffened Shells of Revolution
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-417
一般注記The vibration and buckling characteristics of cantilever truncated conical shells were studied using a finite element computer program for ring-stiffened shells of revolution. For vibration modes having less than two circumferential waves, the frequencies decreased when the size of a support ring at the free end was increased, while, for modes with several circumferential waves, the frequencies initially increased rapidly when the ring size was increased and then became relatively insensitive to further increase in ring size. It was also shown that conditions at the free end have pronounced effects on the buckling external pressure. Results compare favorably with available experimental data.
資料番号: NALTR0417000
レポート番号: NAL TR-417
一次資料へのリンクURLhttps://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=44666&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