I would like to offer this project for UAV CFD (Computational Fluid Dynamics) Analysis for the following:
1. Drag coefficient for different angle of attack
2. Lift coefficient for different angle of attack
3. Drag Polar Diagram
4. Velocity vector, pressure contour and stream lines between wing and fuselage
5. Stream lines to study wing tip vortices
6. Pressure contour on structures
7. Downward vertical velocity component
Hi. I'm an aeronautical engineering student with extensive knowledge in aerodynamics. I also have an extensive knowledge in CFD, mainly with Fluent. See PM for samples.
I'm a graduated Aerospace engineer with a MSc thesis in CFD. It is two year that I work with CFD on daily basis. I think my knowledge and my background match very well the project requirements.
I am a graduate from Cranfield University with specialisation in Aerodynamics. I had done similar projects before. I have knowledge in softwares like ANSYS CFX, FLUENT, TECPLOT. I am sure that I can give you amazing post processing results for this project.