Airfoil Performance and Testing for Fighter Jets with CFD Simulations
Budget: £20 – £250 GBP
This project tests the performance of a specific airfoil on a fighter jet wing using CFD simulations in ANSYS. The airfoil is evaluated to determine if it meets the aircraft’s performance goals, such as speed and maneuverability. The findings will help assess the airfoil’s suitability for the design requirements.
Related categories:
Matlab and Mathematica
Aerospace Engineering
Computational Fluid Dynamics
Aircraft Performance
Ansys