Vertical Drop Test of a YS-11 Fuselage Section
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- Minegishi Masakatsu
- 航空宇宙技術研究所
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- Kumakura Ikuo
- 航空宇宙技術研究所
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- Iwasaki Kazuo
- 航空宇宙技術研究所
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- Shoji Hirokazu
- 航空宇宙技術研究所
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- Yoshimoto Norio
- 航空宇宙技術研究所
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- Terada Hiroyuki
- 航空宇宙技術研究所
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- Sashikuma Hirofumi
- 川崎重工業(株)
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- Isoe Akira
- 川崎重工業(株)
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- Yamaoka Toshihiro
- 川崎重工業(株)
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- Katayama Noriaki
- 川崎重工業(株)
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- Hayashi Toru
- 川崎重工業(株)
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- Akaso Tetsuya
- 川崎重工業(株)
Bibliographic Information
- Other Title
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- YS-11型機胴体構造の落下衝撃試験(その1)
- YS 11ガタキ ドウタイ コウゾウ ノ ラッカ ショウゲキ シケン ソノ 1
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Abstract
The Structures and Materials Research Center of the National Aerospace Laboratory of Japan (NAL) and Kawasaki Heavy Industories, Ltd. (KHI) conducted a vertical drop test of a fuselage section cut from a NAMIC YS-11 transport airplane at NAL vertical drop test facility in December 2001. The main objectives of this program were to obtain background data for aircraft cabin safety by drop test of a full-scale fuselage section and to develop computational method for crash simulation. The test article including seats and anthropomorphic test dummies was dropped to a rigid impact surface at a velocity of 6.1 m/s (20 ft/s). The test condition and result were considered to be severe but potentially survivable. A finite element model of this test article was also developed using the explicit nonlinear transient-dynamic analysis code, LS-DYNA3D. An outline of analytical method and comparison of analysis result with drop test data are presented in this paper.
Journal
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- JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
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JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES 51 (594), 354-363, 2003
THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
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Details 詳細情報について
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- CRID
- 1390282679447308416
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- NII Article ID
- 10011458451
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- NII Book ID
- AA11307372
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- ISSN
- 24323691
- 13446460
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- NDL BIB ID
- 6647326
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- Text Lang
- ja
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- Data Source
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- JaLC
- NDL
- Crossref
- CiNii Articles
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- Abstract License Flag
- Disallowed