並列タイトル等Vertical drop test of a YS-11 fuselage section(Part1)
タイトル（掲載誌）航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory
一般注記The Structures and Materials Research Center of the National Aerospace Laboratory of Japan(NAL) and Kawasaki Heavy Industries, Ltd.(KHI) conducted a vertical drop test of a fuselage section cut from a NAMC YS-11 transport airplane at the NAL vertical drop test facility in December 2001. The main objectives of this testing program were to obtain background data for aircraft cabin safety via a drop test of a full-scale fuselage section, and develop a computational method for crash simulation. The test object including seats and anthropomorphic test dummies was dropped onto a rigid impact surface at a velocity of 6.1 m/s (20 ft/s). Comparing the pelvic loads of the test dummies and limitations of the load defined in the Federal Airworthiness Regulations for emergency landings, the drop test conditions (impact velocity) of the test object were found to be severe, but survivable for passengers. A finite element model of this test object was also developed using the explicit nonlinear transient-dynamic analysis code, LS-DYNA 3D. An outline of the analytical method and comparative analysis using drop test data are presented in this paper.
資料番号: AA0046107000
レポート番号: NAL TR-1461
一次資料へのリンクURLhttps://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=42863&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