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update mfoil link and add reference #14

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aeronauty-flexcompute merged 1 commit into from
Mar 25, 2026
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update mfoil link and add reference #14

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1 change: 1 addition & 0 deletions README.md
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Expand Up @@ -158,6 +158,7 @@ const solution = foil.solve();
1. Drela, M. "XFOIL: An Analysis and Design System for Low Reynolds Number Airfoils" (1989)
2. Katz, J. & Plotkin, A. "Low-Speed Aerodynamics" (2001)
3. Cebeci, T. & Bradshaw, P. "Momentum Transfer in Boundary Layers" (1977)
4. Fidkowski, K. J. "A Coupled Inviscid-Viscous Airfoil Analysis Solver, Revisited," *AIAA Journal*, Vol. 60, No. 5, 2022, pp. 2961–2971. [doi:10.2514/1.J061341](https://doi.org/10.2514/1.J061341)

## License

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3 changes: 2 additions & 1 deletion THIRD_PARTY_NOTICES.md
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Expand Up @@ -47,7 +47,7 @@ TypeWithKnife.
- **Path:** `mfoil/mfoil.py`
- **Author:** Krzysztof J. Fidkowski
- **License:** MIT
- **Source:** <https://github.com/kjfid/mfoil>
- **Source:** <https://websites.umich.edu/~kfid/codes.html>
- **Description:** Python-based airfoil analysis code used as a reference
implementation during development.

Expand All @@ -63,3 +63,4 @@ contain any XFOIL source code. The mathematical methods are documented in:
Airfoils" (1989)
- Drela, M. & Giles, M. B. "Viscous-Inviscid Analysis of Transonic and Low
Reynolds Number Airfoils" (1987)

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