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Program Foil CFD :

Solving The Entire Steady Incompressible Subsonic Flow Field About Two Dimensional Lifting And Non-Lifting Surfaces , By Integrating The Ordinary Differential Elliptic Laplace Equation Describing The Velocity Function , Over A Delaunay Triangular Grid Using The Numerical Dormand-Prince Fifth Order Integrator , With Neumann Boundary Conditions

 

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