Actuator line modeling for OpenFOAM.
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Updated
Apr 4, 2026 - C++
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airfoils
Here are 2 public repositories matching this topic...
PANKH (Panel Analysis of uNsteady Kinematics of Hovering airfoils) is a solver for studying unsteady aerodynamics of flapping and hovering airfoils using the unsteady vortex panel method. This repository includes the source code, example cases, and validation results.
airfoils unsteady-flows naca potential-flow-theory vortex-panel-method kutta-schukowski kutta-condition
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Updated
Nov 10, 2025 - C++
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