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1)
https://jaxa.repo.nii.ac.jp/records/42863
https://jaxa.repo.nii.ac.jp/records/42863b9d66b33-ea04-4262-8dca-6fd365869f30
名前 / ファイル | ライセンス | アクション |
---|---|---|
naltr0001461.pdf (12.6 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1) | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | YS-11胴体部 | |||||
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 | 航空機キャビン安全性 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | クラッシュ着陸 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 計算機シミュレーション | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | FEM | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 剛体衝突面 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 人間試験人形 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 衝突速度 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 研究開発 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | YS-11 fuselage section | |||||
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 cabin safety | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | crash landing | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | computerized simulation | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | FEM | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | rigid impact surface | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | anthropomorphic test dummy | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | impact velocity | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | research and development | |||||
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(Part1) | |||||
著者 |
峯岸, 正勝
× 峯岸, 正勝× 岩崎, 和夫× 熊倉, 郁夫× 少路, 宏和× 吉本, 周生× 寺田, 博之× 指熊, 裕史× 磯江, 暁× 山岡, 俊洋× 片山, 範明× Minegishi, Masakatsu× Iwasaki, Kazuo× Kumakura, Ikuo× Shoji, Hirokazu× Yoshimoto, Norio× Terada, Hiroyuki× Sashikuma, Hirofumi× Isoe, Akira× Yamaoka, Toshihiro× Katayama, Noriaki |
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著者所属 | ||||||
航空宇宙技術研究所 構造材料研究センター | ||||||
著者所属 | ||||||
航空宇宙技術研究所 構造材料研究センター | ||||||
著者所属 | ||||||
航空宇宙技術研究所 構造材料研究センター | ||||||
著者所属 | ||||||
航空宇宙技術研究所 構造材料研究センター | ||||||
著者所属 | ||||||
航空宇宙技術研究所 構造材料研究センター | ||||||
著者所属 | ||||||
航空宇宙技術研究所 業務部 | ||||||
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 | ||||||
川崎重工業 | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory Structures and Materials Research Center | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory Structures and Materials Research Center | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory Structures and Materials Research Center | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory Structures and Materials Research Center | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory Structures and Materials Research Center | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory Operations and External Relations Division | ||||||
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. | ||||||
著者所属(英) | ||||||
en | ||||||
Kawasaki Heavy Industries Ltd. | ||||||
出版者 | ||||||
出版者 | 航空宇宙技術研究所 | |||||
出版者(英) | ||||||
出版者 | National Aerospace Laboratory (NAL) | |||||
書誌情報 |
航空宇宙技術研究所報告 en : Technical Report of National Aerospace Laboratory 巻 1461, 発行日 2003-06 |
|||||
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) 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. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 1347-4588 | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AN00311347 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0046107000 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: NAL TR-1461 |