Program Super Foil :

Solves the subsonic inviscid flow field , and the supersonic viscous flow field , about arbitrary airfoils , using six mathematical models

Geometry Module :

• One series airfoils
• Four series airfoils , standard and modified thickness
• Five series airfoils , standard and modified thickness
• Five series reflexed airfoils , standard and modified thickness
• Six series airfoils , standard and modified mean lines
• Joukowski airfoils
• Von-Karman airfoils
• Variable axes sections
• Saved library of 1420 different airfoil file
• Four paneling schemes (normal distribution , full cosine spacing , half sine spacing , half cosine spacing )

Grid Module :

• Flat panels on the mean line
• Flat panels on the complete outer surface
• Unstructured triangular grid , for the full domain inviscid solver
• Structured elliptic partial differential grid , for the supersonic viscous solver

Aerodynamic Module :

• Analytic thin airfoil theory

• Numerical lumped vortex panel method

• Numerical constant sources + constant vortex panel method

• Numerical linear vortex panel method

• Computational integration of the potential flow equation in full-domain , using 5'th order dormand-prince integrator on triangular grid

• Supersonic compressible viscous Navier-Stokes equations , using the numerical time marching accurate Maccormack finite difference method on elliptic grid