Numerical Investigation of Toggle Assembly of Landing Gears in Aircraft: Technical note

Gopalakrishnan, T. and Saravanan, R. and Karunakaran, K. (2019) Numerical Investigation of Toggle Assembly of Landing Gears in Aircraft: Technical note. International Journal of Vehicle Structures and Systems, 11 (2). ISSN 0975-3060

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Abstract

Numerical Investigation of Toggle Assembly of Landing Gears in Aircraft: Technical note T. Gopalakrishnan R. Saravanan K. Karunakaran

In aircraft design functional components are of top priority. This numerical investigation is used for evaluating the fulfilment of strength requirement of the landing gear toggle assembly. The landing gear is the structure which supports the aircraft and helps in taxiing, take-off and landing of the aircraft. Hence it is suffered by more fatigue load than the other applications. The replacement of steel to aluminium was investigated. Every part is individually analysed and its part with sub-assemblies also investigated.
08 12 2019 10.4273/ijvss.11.2.17 https://yanthrika.com/eja/index.php/ijvss/article/view/1223 https://yanthrika.com/eja/index.php/ijvss/article/download/1223/578 https://yanthrika.com/eja/index.php/ijvss/article/download/1223/578

Item Type: Article
Subjects: Naval Architecture and Offshore Engineering > Naval Architecture
Divisions: Naval Architecture and Offshore Engineering
Depositing User: Mr IR Admin
Date Deposited: 06 Oct 2024 06:34
Last Modified: 06 Oct 2024 06:34
URI: https://ir.vistas.ac.in/id/eprint/8809

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