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- W2891550814 abstract "Contact between two objects is an important facet in multibody dynamics. It is a discontinuous, non-linearphenomenon and consequently it requires iterative simulations. The paper presents the reliability evaluation of theretraction landing gear mechanism by three contact models Viz. Impact Function Model, Coefficient of Restitution Modeland Clearance Link Model. The simulations have been performed using the standard commercial multibody dynamicssoftware ADAMS. The precision of these simulations depends on user-defined parameters like stiffness, Damping,Penetration Depth, Force exponent, Penalty and Restitution Coefficient that impacts the overall reliability of themechanism. The optimal value of these parameters have been obtained by an optimization process using Design ofExperiments tool available in ADAMS to match with the nominal values without any clearance.. The overall reliability ofthe mechanism has been evaluated at different instants of the retraction cycle by using Response Surface Based MonteCarlo Simulation and Direct Monte Carlo Simulation by using in house codes created in MATLAB software. Thecomparison, significance and accuracy of the results obtained using the above -mentioned approaches has been discussedand the impact based contact modelling for the clearance appears to be accurate and realistic for practical applications." @default.
- W2891550814 created "2018-09-27" @default.
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- W2891550814 date "2016-01-01" @default.
- W2891550814 modified "2023-09-24" @default.
- W2891550814 title "Reliability studies on the influence of joint clearance on the kinematics of the nose landing gear mechanism of a transport aircraft using contact theory" @default.
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- W2891550814 hasPublicationYear "2016" @default.
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