淡江大學機構典藏:Item 987654321/96899
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    Please use this identifier to cite or link to this item: https://tkuir.lib.tku.edu.tw/dspace/handle/987654321/96899


    Title: Impact Loading Analysis of Light Sport Aircraft Landing Gear
    Authors: Chen, Pu-Woei;Chang, Shu-Han;Chen, Chan-Ming
    Contributors: 淡江大學航空太空工程學系
    Keywords: Light sport aircraft;Landing gear;Impact test
    Date: 2014-02-28
    Issue Date: 2014-03-14 09:45:59 (UTC+8)
    Publisher: Stafa-Zurich: Trans Tech Publications
    Abstract: This paper examined the critical loading condition of a light sport aircrafts main landing gear during the impact loading condition. The new category airplane was established by the FAA in 2004. The light sport aircraft has great market demand for personnel entertainment purpose and regional transportation. The main object of this research was to establish a static and dynamic loading simulation model for the aluminum alloy landing gear of a light sport aircraft. This work also examined the critical loading parameters of the main landing gear, including the maximum take-off weight and maximum stall speed. The analysis was performed using ANSYS and LS-DYNA to establish the finite element model after simplifying the geometric characteristics and verifying the results by energy conservation, hourglass energy, and sliding energy. The study tested aluminum plates with a thickness from 15~25 mm. The results showed all the samples could sustain the required loading condition, except for the thickness of 15mm that failed under impact loading. The simulation model provides a cost-saving process compared to a real crashworthiness drop test to test the main landing gears compliance with regulations.
    Relation: Applied Mechanics and Materials 518, pp.252-257
    DOI: 10.4028/www.scientific.net/AMM.518.252
    Appears in Collections:[Graduate Institute & Department of Aerospace Engineering] Journal Article

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