MATLAB Implementation for Aircraft Design with Complete Workflow

Comprehensive aircraft design program covering complete workflow including overall aircraft parameters, aerodynamic curves, wing loading analysis, and propeller characteristics with computational implementation details.

Aircraft Design as an Iterative Process Requiring Multiple Computations

Aircraft design is an iterative process that requires multiple cycles and extensive computations. To address this, we have developed several MATLAB programs. The source code for these programs is available through the links below: [program_1.m] Overall Aircraft Parameter Calculation Program, [program_2.m] Aircraft Aerodynamic Curve Calculation Program, [program_3.m] Wing Load Distribution Calculation Program, [program_4.m] Longitudinal Dynamic Stability Calculation Program for Cruise Conditions, [program_5.m] Lateral-Directional Stability Calculation Program, [program_6.rar] Level Flight Speed Range Calculation Program, [program_7.rar] Propeller Characteristics Calculation Program.