* 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.

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