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

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

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 d...

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Veröffentlicht in:Russian aeronautics 2020-12, Vol.63 (4), p.586-593
Hauptverfasser: Mikhailov, A. A., Keresten’, I. A., Nikitin, M. A., Voinov, I. B., Morozov, D. I.
Format: Artikel
Sprache:eng
Schlagworte:
Automotive Engineering
Engineering
Flight Vehicle Design
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Zusammenfassung: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.
ISSN:1068-7998
1934-7901
DOI:10.3103/S1068799820040042