著者
少路 宏和
出版者
一般社団法人 日本航空宇宙学会
雑誌
日本航空宇宙学会誌 (ISSN:00214663)
巻号頁・発行日
vol.53, no.617, pp.182-187, 2005-06-05 (Released:2019-04-17)
参考文献数
30
被引用文献数
1
著者
峯岸 正勝 熊倉 郁夫 岩崎 和夫 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 林 徹 赤楚 哲也
出版者
一般社団法人 日本航空宇宙学会
雑誌
日本航空宇宙学会論文集 (ISSN:13446460)
巻号頁・発行日
vol.51, no.594, pp.354-363, 2003 (Released:2003-09-26)
参考文献数
19
被引用文献数
1 2

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.