Design analysis of Landing gear system of an aircraft

This paper mainly focuses on understanding the working principle of the landing gear of an aircraft and also cover various types and configuration of landing gears used in the aircraft industry. Furthermore this research includes the design and analysis of the landing gear system, using software such as CATIA V5 and ANSYS. The secondary objective is to optimize each system and the failures experienced by them, along with meeting the challenges and providing innovative methods to improve the existing functioning of the landing gear system.