Program FastFoil :
Using Four Different Analytical And numerical Concentrated And Surface Distribution Potential Flow Solvers , To Calculate The Inviscid Two Dimensional Lifting And Non-Lifting Airloads
Program Abilities :
- Reads Airfoil Coordinate File
- Spline Interpolation To Renumber And Rescale The Airfoil
- Calculates The Camber Line Ordinates
- Aerodynamic Solvers :
- The Classical Thin Airfoil Theory
- Lumped Vortex Concentrated Distribution Panel Method
- Constant Source & Constant Vortex Surface Distribution Panel Method
- Linear Vortex Surface Distribution Panel Method
- Writes Geometry And Results To A Text File