Structural Strength Analysis and Optimization of Commercial Aircraft Nose Landing Gear under Towing Taxi-Out Conditions Using Finite Element Simulation and Modal Testing

In the field of civil aviation, the nose landing gear is a critical component that is prone to damage during taxiing. With the advent of new technologies such as towing taxi-out and hub motors, the nose landing gear faces increasingly complex operational environments, thereby imposing higher perform...

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Autors principals:	Qiwei Lin, Chang Yang, Yuhao Bai, Jiahao Qin
Format:	Artigo
Idioma:	Inglês
Publicat:	MDPI AG 2024-05-01
Col·lecció:	Aerospace
Matèries:	towing taxi-out nose landing gear finite element simulation modal testing dynamics topological optimization
Accés en línia:	https://www.mdpi.com/2226-4310/11/5/414
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