Design and Analysis of Aircraft wings

Job ID: 31214465

Budget: ₹100 – ₹400 INR

The objective of the project is to enhance the operational aerodynamic characteristics of
newly designed wing through hybridization technique using Optimized Airfoils.Optimized airfoil
improves the lift performances and increases the operating rangebyshifting thestallmargin of a
commercial aircraft wing.
Related categories: Solidworks CATIA Ansys 3D CAD