A stability calculator for RC airplanes which uses an iterative approach to optimize for stability and get the parameters in range for the competition requirements
Main inputs
- Wing area, aspect ratio
- Center of Gravity as a percentage of Mean Aerodynamic Chord
- Tail area, aspect ratio
- Mach number
Main outputs
- Moment arm length
- Wing 3D coefficient of lift slope
- Tail 3D coeefficient of lift slope