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