DESIGN AND ANALYSIS OF AEROFOIL WING WITH AND WITHOUT WINGLET

An aircraft wing structure consists of skin, ribs and spar sections. The spar carries flight loads and the weight of the wings while on the ground. Other structural and forming members such as ribs are attached to the spars, with stressed skin. The wings are the most important lift producing part of the aircraft. The design of wings may vary according to the type of aircraft and its purpose.

Design work carried out are:

The structural parameters of

• Total Deformation
• Von-mises stress
• Shear stress
• Shear intensity

The modal analysis carried out are

• mode shape
• 6 modes of vibrations

Software used:

• CATIA
• ANSYS (CFD)

Project Cost:

Rs. 15000 /-