WEKO3
アイテム
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YS-11型機胴体構造の落下衝撃試験(その2)
https://jaxa.repo.nii.ac.jp/records/2410
https://jaxa.repo.nii.ac.jp/records/24103cd969e2-f65a-4a16-8500-ca1f03da0a67
名前 / ファイル | ライセンス | アクション |
---|---|---|
47402000.pdf (14.5 MB)
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Item type | テクニカルレポート / Technical Report(1) | |||||
---|---|---|---|---|---|---|
公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | YS-11型機胴体構造の落下衝撃試験(その2) | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 胴体 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | YS-11 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 垂直落下試験 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 航空機安全性 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 航空機事故 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 数値シミュレーション | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 動的解析 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 非線形システム | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | fuselage | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | YS-11 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | vertical drop test | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | aircraft safety | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | aircraft accident | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | numerical simulation | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | dynamic analysis | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | nonlinear system | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_18gh | |||||
資源タイプ | technical report | |||||
その他のタイトル(英) | ||||||
その他のタイトル | Vertical drop test of a YS-11 fuselage section(Part 2) | |||||
著者 |
岩崎, 和夫
× 岩崎, 和夫× 峯岸, 正勝× 少路, 宏和× 宮木, 博光× 吉本, 周生× 寺田, 博之× 熊倉, 郁夫× 片山, 範明× 林, 徹× 小坂, 英之× Iwasaki, Kazuo× Minegishi, Masakatsu× Shoji, Hirokazu× Miyaki, Hiromitsu× Yoshimoto, Norio× Terada, Hiroyuki× Kumakura, Ikuo× Katayama, Noriaki× Hayashi, Toru× Kosaka, Hideyuki |
|||||
著者所属 | ||||||
宇宙航空研究開発機構 総合技術研究本部 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 総合技術研究本部 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 総合技術研究本部 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 総合技術研究本部 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 総合技術研究本部 | ||||||
著者所属 | ||||||
航空宇宙技術振興財団 | ||||||
著者所属 | ||||||
東京ビジネスサービス | ||||||
著者所属 | ||||||
川崎重工業 | ||||||
著者所属 | ||||||
川崎重工業 | ||||||
著者所属 | ||||||
川崎重工業 | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Institute of Space Technology and Aeronautics | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Institute of Space Technology and Aeronautics | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Institute of Space Technology and Aeronautics | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Institute of Space Technology and Aeronautics | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Institute of Space Technology and Aeronautics | ||||||
著者所属(英) | ||||||
en | ||||||
Foundation for Promotion of Japanese Aerospace Technology | ||||||
著者所属(英) | ||||||
en | ||||||
Tokyo Business Service Co. Ltd. | ||||||
著者所属(英) | ||||||
en | ||||||
Kawasaki Heavy Industries Ltd. | ||||||
著者所属(英) | ||||||
en | ||||||
Kawasaki Heavy Industries Ltd. | ||||||
著者所属(英) | ||||||
en | ||||||
Kawasaki Heavy Industries Ltd. | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構 | |||||
出版者(英) | ||||||
出版者 | Japan Aerospace Exploration Agency (JAXA) | |||||
書誌情報 |
宇宙航空研究開発機構研究開発報告 en : JAXA Research and Development Report 巻 JAXA-RR-03-010, 発行日 2004-03-25 |
|||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | The Structures and Materials Research Center of the National Aerospace Laboratory of Japan (NAL) in conjunction with Kawasaki Heavy Industries, LTD (KHI) conducted a second vertical drop test of a fuselage section cut from a NAMC YS-11 transport airplane in July 2002. The main objective of this test program was to obtain background data for aircraft cabin safety by drop testing a full-scale fuselage section, and to develop a computational tool for aircraft fuselage structure crash simulation. The test article including seats and anthropomorphic test dummies was dropped onto a rigid impact surface using the free-fall method at a velocity of 7.6 m/s (25 ft/s). The impact environment and the resultant response of the fuselage structure and the passenger dummies were considered to be severe but potentially survivable. Finite element models of the test articles for vertical drop tests were developed using a nonlinear dynamic analysis code, LS-DYNA3D. Correlation between test and analysis was fairly good. A description of some of the results of the full-scale fuselage section drop tests and numerical simulations is presented in this paper. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 1349-1113 | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AA1192675X | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0047402000 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: JAXA-RR-03-010 |