* Generating 3D finite element mesh for canard-wing-tail-body combination.
* Full or half 3D mesh and corresponding initial and boundary conditions.
* Hybrid finite element meshes: Hexahedral, Prism, Tetrahedral and Pyramid.
* Unique flow solver to solve flow problems with the above hybrid finite element meshes.
Euler or Navier Stokes equations.
* Double circular arc, double wedge (a=1/2) or modified double wedge (a=1/3),
NACA airfoil or elliptical wing sections.