Linear Vortex Panel Method in MATLAB
This project is about implementing a MATLAB code to find the pressure coefficient distribution over an airfoil using Linear Vortex Panel method. It can be used for any airfoil. It is only needed to use an airfoil generator and insert the data of the airfoil into the code to get the Cp distribution.
About Me
I'm a PhD aerospace engineering researcher and a teaching assistant at university of Connecticut. My masters was in aerodynamics and CFD. I also have strong command in some programming languages. Experience:- ----------------- -3 years of experience in modeling and visualizing flow fields in automotive industries (ANSYS / OpenFOAM / FEMAP). -I worked for 6 months as a mathematician. -5 months of experience in solidworks and autocad. Skills :- ----------------- - CFD and hypersonics. - Jet and rocket engines. - Orbital mechanics engineer and space mission analyst. - Aerodynamics and Heat transfer. - Python, C/C++, Fortran, mathematica and MATLAB/SIMULINK.