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[![Dev](https://img.shields.io/badge/docs-dev-blue.svg)](https://Albatross-Kite-Transport.github.io/VortexStepMethod.jl/dev) [![Build Status](https://github.com/Albatross-Kite-Transport/VortexStepMethod.jl/actions/workflows/CI.yml/badge.svg?branch=main)](https://github.com/Albatross-Kite-Transport/VortexStepMethod.jl/actions/workflows/CI.yml?query=branch%3Amain) [![Coverage](https://codecov.io/gh/Albatross-Kite-Transport/VortexStepMethod.jl/branch/main/graph/badge.svg)](https://codecov.io/gh/Albatross-Kite-Transport/VortexStepMethod.jl)
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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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