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Approximating the Circulation along the span wise axis for a Finite Length Wing using Prandtl Lifting-Line theory.

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Name		Name	Last commit message	Last commit date
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README.md		README.md
example_code.py		example_code.py
finite_wing.py		finite_wing.py
plot_functions.py		plot_functions.py
wings.py		wings.py

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Finite_Wing

Approximating the Circulation along the span wise axis for a Finite Length Wing using Prandtl Lifting-Line theory.

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Approximating the Circulation along the span wise axis for a Finite Length Wing using Prandtl Lifting-Line theory.

python3 finite-element-analysis aerodynamics prandtl-liftingline finite-wing

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