Design and Analysis of Landing Gear using Composite Material

Abstract

Aircraft frames are supported physically by the system of assembly which is an important component of aircraft which helps in transferring the load bearded by the wing to the ground while landing this is known as landing gear therefore it is a vital part to construct a landing gear which could withstand external force and could show least deformation the experimental structural analysis conducted was to find the best alternate of titanium alloy mainly used for the manufacturing of triple bogey type of landing gear the structural  analysis of landing gear which was designed in solid works has been analysed using the Ansys software from the obtained data we can  understand least deformation shown by composite AL Sic.