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# Simulation of a 3D airfoil using the Vortex Step Method
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# Simulation of a 3D wing using the Vortex Step Method
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The Vortex Step Method (VSM) is an enhanced lifting line method that improves upon the classic approach by solving the circulation system at the three-quarter chord position, among the most important details. This adjustment allows for more accurate calculations of lift and drag forces, particularly addressing the shortcomings in induced drag prediction.
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VSM is further refined by coupling it with 2D viscous airfoil polars, making it well-suited for complex geometries,
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