Verification of stress concentration theory
The purpose of this project is to restraining the shaft from moving in the radial and axial direction to determine realistic locations for both maximum stress and
displacement using finite element analysis.
FEA OF LANDING GEAR OF BOEING 747-400
The purpose of this project is to analyzing the Oleo cylinder of the Nose Landing gear of the Boeing 747-400 and run FEM analysis to validate the design structural integrity. In this project, stress analysis of Oleo cylinder was evaluated using Solidworks COSMOS Simulation and result were used to optimize the critical stress.
