Standard Airfoil Coordinate Generation with Aerodynamic Analysis

This software enables generation of standard airfoil coordinate data through parametric algorithms and coordinate transformation methods. Beyond coordinate generation, it performs comprehensive aerodynamic calculations including lift coefficient (CL) and drag coefficient (CD) analysis at multiple angles of attack using panel methods or computational fluid dynamics (CFD) approximations. The system incorporates additional functionalities for airfoil profile design through Bézier curves or NACA series algorithms, along with advanced airfoil characteristic analysis modules. Key computational features include boundary layer integration, pressure distribution calculations, and performance optimization routines. Through its integrated toolset, users can efficiently conduct airfoil design and analysis workflows, significantly enhancing productivity in aircraft design processes with automated mesh generation and results visualization capabilities.