The following MATLAB script files contain code that may be useful for solving engineering problems encountered in the field of Aeronautics.

- Function to calculate air density for given altitude
- Sample aircraft range calculation (Boeing 737-300)
- Specific Excess Power Contours for Aircraft Performance Calculations
- Blade Element Theory Calculation for Propellers
- A Two dof System for Simple Flutter Prediction
- A randon walk simulation of Two Phase Flow (point Source).