Implement a default inviscid polar

ocayon / Vortex-Step-Method

Vortex Step Method

MIT License

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Implement a default inviscid polar #12

Closed jellepoland closed 2 months ago

jellepoland commented 2 months ago

Whenever the user does not provide any aerodynamic characteristics of the airfoil in 2D, the code should still run with CL = 2PI and zero viscous drag.