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Parametric Analysis on Landing Gear Strut Friction of Light Aircraft for Touchdown Performance

The aim of this paper is to obtain the strut friction–touchdown performance relation for designing the parameters involving the strut friction of the landing gear in a light aircraft. The numerical model of the landing gear is validated by drop test of single half-axle landing gear, which is used to...

Disgrifiad llawn

Wedi'i Gadw mewn:
Manylion Llyfryddiaeth
Prif Awduron: Shengyong Gan, Xingbo Fang, Xiaohui Wei
Fformat: Artigo
Iaith:Inglês
Cyhoeddwyd: MDPI AG 2021-06-01
Cyfres:Applied Sciences
Pynciau:
Mynediad Ar-lein:https://www.mdpi.com/2076-3417/11/12/5445
Tagiau: Ychwanegu Tag
Dim Tagiau, Byddwch y cyntaf i dagio'r cofnod hwn!