教師資料查詢 | 類別: 期刊論文 | 教師: 陳步偉 CHEN PU-WOEI (瀏覽個人網頁)

標題:Crashworthiness Simulation Analysis of Light Sport Aircraft Fuselage Structure
學年99
學期2
出版(發表)日期2011/02/01
作品名稱Crashworthiness Simulation Analysis of Light Sport Aircraft Fuselage Structure
作品名稱(其他語言)
著者Chen, Pu-woei; Chang, Shu-han; Hsieh, Yu-yang; Sun, Tai-sing
單位淡江大學航空太空工程學系
出版者Stafa-Zurich: Trans Tech Publications Ltd.
著錄名稱、卷期、頁數Advanced Materials Research 199-200, pp.48-53
摘要In recent years, light sport aircraft, which not only serve the purpose of personal recreation but also act as a means of transportation for medium and short distance travel, have rapidly gained popularity in the general aviation industry worldwide. The FAA established regulations for this new category of airplanes in 2004. However, the crashworthiness requirements for this type of airplane have not been clearly specified. This study used the finite element method to investigate the effect of the impact angle and speed of the LSA fuselage structure on passenger safety during a crash event. We used sink speed defined by NASA AGATE, ASTM and FAR as parameters. The passenger compartment reducing rate defined by MIL-STD-1290A was used for a safety boundary condition. The results show that the maximum cockpit reducing rate of the airplane impact angle is 30o. When the impact angle increases, owing to the engine mount and fire wall’s reinforced structure, this type of airplane can sustain a greater vertical drop speed. When the impact angle is about 80°~90°, the maximum impact speed the fuselage that can be sustained is 33 m/s. This work also completed a simulation of safe and unsafe ranges for light sport aircraft at various impact angles and vertical drop speeds during impact.
關鍵字Light Sport Aircraft; Crashworthiness; Finite Element Analysis
語言英文
ISSN1022-6680
期刊性質國外
收錄於SCI;EI
產學合作
通訊作者
審稿制度
國別瑞士
公開徵稿
出版型式紙本
相關連結
Google+ 推薦功能,讓全世界都能看到您的推薦!