A point-source boundary condition is required for accurate drag at high incidence, and a simple Lagally-Filon correction approximates it for blocked sidewalls.
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Far-field Boundary Conditions for Airfoil Simulation at High Incidence in Steady, Incompressible, Two-dimensional Flow
A point-source boundary condition is required for accurate drag at high incidence, and a simple Lagally-Filon correction approximates it for blocked sidewalls.