About the Landing Gear Design Experience for a Light Aircraft Based on Multidisciplinary Modeling

A. A. Mikhailov,I. A. Keresten’, M. A. Nikitin, I. B. Voinov, D. I. Morozov

Russian Aeronautics（2021）

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Abstract

In this paper, the numerical simulation approach for designing the landing gear strut for a light aircraft is presented. The problems of extension and compression of the landing gear, as well as its strength during landing, are considered. The application of the topological optimization method for determining the optimal landing gear strut shape is shown.

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Key words

landing gear strut,strength,landing,numerical engineering,stress-strain state,finite element method,topological optimization

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