Objective

• The scope of this project is to identify the behavior of Wing, after modifying several structural components like Ribs, Spars in analysis interface Ansys.
  

  Various Load conditions and directions are considered from previous model.
  

Accomplishments

• Calculated the strength of the Wing by applying various loads in several directions as per the functioning and requirement of the customer.
  

  Pressure and Temperature loads mapped from 2D Global model.
  

  Von mises stress analysis, deformation calculation is done in Ansys interface.