Select a material, skins thicknesses and standard cross-section dimensions to produce a 1.5
minimum margin of safety.
• Build an excel sheet for the analytical solution based on the beam theory that can obtain wing
stresses, margin of safety, member forces, beam deformations.
• Solve the same wing using ANSYS workbench.
• Compare between the analytical and finite element solutions in point of view of stresses, forces,
• Apply some parametric study such as the effect of adding ribs, making cutouts, changing skin and
web thicknesses, changing stringers areas, heights, or thickness and so on.
This project needed to be completed before Jan 12 midnight.
If you're interested, apply and I'll send any needed further details.
18 freelancers are bidding on average $159 for this job
Hello sir, I'm mechanical engineer will use ansys and solve your task I'm expert in this kind of work I'm also using software like, Solidwork Autocad ansys FEA CFD 3d modelling waiting to here from you