I will write python or matlab scripts for aerodynamic analysis

I'll turn your aerodynamics, fluid dynamics, or numerical engineering problem into a working Python or MATLAB script clean code, clear results, and a plain-language explanation of what the numbers mean.

I'm an aerospace engineering graduate student with hands-on experience in computational fluid dynamics, airfoil and propeller aerodynamics, and numerical simulation methods. I work in Python (numpy, scipy, matplotlib) and MATLAB, using open-source aerodynamics tools like XFOIL for airfoil analysis and blade element momentum theory for propeller and rotor performance.

What I can help with:

• Airfoil aerodynamic analysis (lift, drag, moment coefficients across angle-of-attack ranges)
• Propeller and rotor performance analysis using blade element momentum (BEM) theory
• Custom numerical solvers (root-finding, ODE/PDE integration, iterative methods)
• Data processing and visualization for simulation or experimental results
• Clean, readable Python/MATLAB code you can actually modify afterward

What this isn't: GUI-based commercial CFD setup or meshing (ANSYS Fluent, CATIA, etc.) my focus is script-based analysis and numerical methods, not point-and-click software operation.