Difference Algorithm of the Posture of Airliner Forced Landing onto Water in Bowing Stage

By using solid-fluid coupling, momentum conservation, motion equation and pressure drag, a difference algorithm is employed to find the posture of airliner landing onto water in bowing stage for the different angle. The results show that the final velocity is positive correlated with impact angle wh...

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Veröffentlicht in:Applied Mechanics and Materials 2012-05, Vol.170-173, p.1987-1990
Hauptverfasser: Zhang, She Sheng, Huang, Yan, Zhan, Dong Wen, Tao, Ze Feng
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container_end_page 1990
container_issue
container_start_page 1987
container_title Applied Mechanics and Materials
container_volume 170-173
creator Zhang, She Sheng
Huang, Yan
Zhan, Dong Wen
Tao, Ze Feng
description By using solid-fluid coupling, momentum conservation, motion equation and pressure drag, a difference algorithm is employed to find the posture of airliner landing onto water in bowing stage for the different angle. The results show that the final velocity is positive correlated with impact angle when the angle is less than 80; the final velocity is negative correlated with impact angle when the angle is more than 80, waves make the immersed part decrease, which leads to a buoyancy reduction and acceleration increment.
doi_str_mv 10.4028/www.scientific.net/AMM.170-173.1987
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title Difference Algorithm of the Posture of Airliner Forced Landing onto Water in Bowing Stage
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