MODELING AND SIMULATION ANALYSIS OF AIRCRAFT WING LOADS

The analysis, implementation and modeling of aircraft wing's charges are presented. The integration of different mathematical equations is described to identify each load that acts on the wing structure for the sake of obtaining the overall load profile. Then, the load profile is calculated by combining the physical and geometrical parameters namely lift load, wing and fuel weights which act on the wing. This developed model analytically points out the critical parameters that influence the system's behavior. Additionally, numerical analysis is carried out using finite element analysis to obtain pressure distribution, von mises stress and displacement. Finally, the obtained results are graphically represented and discussed through Matlab environment.