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DDES Simulation of a Complex Main Landing Gear with Six-Wheel Bogie
34th AIAA Applied Aerodynamics Conference, 2016This paper investigates numerically the flow and unsteady aerodynamics of a complex landing gear using Delayed Detached Eddy Simulation (DDES). The case studied is a six-wheel main landing gear with some medium and small components included, which has been measured previously in wind tunnel.
Utsav Oza, Zhiwei Hu, Xin Zhang
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Fatigue analysis of a P180 aircraft main landing gear wheel flange
Engineering Failure Analysis, 2008Abstract A piece of inner wheel flange separated from the main landing gear (MLG) right wheel of a Piaggio Avant P180 aircraft during taxing on the runway. The wheel was a 2014-T6 aluminium alloy and had been in service 22 years. Morphological observation of the fractured surfaces indicated fatigue was the cause of failure.
F. Bagnoli, M. Bernabei
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The Reduction of Main Landing Gear Noise
22nd AIAA/CEAS Aeroacoustics Conference, 2016John Kennedy +2 more
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Fatigue Crack Growth in Aircraft Main Landing Gear Wheels
1988Fracture analysis of aircraft landing gear wheels under service-simulated operating loads using various fatigue crack growth characterization techniques is presented. Baseline constants for the wheel forging alloy 2014-T6 aluminum are established. The stress-intensity factors for a two-dimensional surface crack are developed using a proposed load model
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Modelling and Simulation of an Aircraft Main Landing Gear Shock Absorber
2015Every traditional aircraft has a shock absorber in its main landing gear. A shock absorber takes the brunt of the shock imparted to the landing gear, absorbs it and dissipates the kinetic energy. This thesis is based on the construction of a realistic analytical model of an oleo-pneumatic shock absorber for a combat aircraft.
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Research on Landing Stability of Four-Legged Adaptive Landing Gear for Multirotor UAVs
Aerospace, 2022Xiaohui Wei, Wei Xiaohui
exaly
Experimental Validation for the Performance of MR Damper Aircraft Landing Gear
Aerospace, 2021Jai-Hyuk Hwang
exaly
Main Landing Gear Conceptual Design and Analysis for M.A.L.E U.C.A.V
2021 Seventh International Conference on Aerospace Science and Engineering (ICASE), 2021Asim Mehmood +3 more
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Noise reduction technologies for aircraft landing gear-A bibliographic review
Progress in Aerospace Sciences, 2020Kun Zhao +2 more
exaly
Generative design of main landing gear for a remote-controlled aircraft
Materials Today: Proceedings, 2023Aditya Gupta +3 more
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