MATLAB Implementation for Aircraft Design - Key Computational Programs and Algorithms

Comprehensive aircraft design suite featuring MATLAB programs for overall parameter calculation, full-aircraft aerodynamic curve computation, wing load distribution analysis, longitudinal dynamic stability assessment in cruise, lateral-directional stability evaluation, level flight speed range determination, and propeller characteristic modeling with detailed algorithm explanations.

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.