From 38e3a4d5260790a38d30fe358129d06f84cb6843 Mon Sep 17 00:00:00 2001 From: awccoppFC Date: Wed, 25 Mar 2026 13:55:13 -0400 Subject: [PATCH] update mfoil link and add reference --- README.md | 1 + THIRD_PARTY_NOTICES.md | 3 ++- 2 files changed, 3 insertions(+), 1 deletion(-) diff --git a/README.md b/README.md index 465d29f0..5f0d77c2 100644 --- a/README.md +++ b/README.md @@ -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 diff --git a/THIRD_PARTY_NOTICES.md b/THIRD_PARTY_NOTICES.md index 4bb9f01f..9f24c224 100644 --- a/THIRD_PARTY_NOTICES.md +++ b/THIRD_PARTY_NOTICES.md @@ -47,7 +47,7 @@ TypeWithKnife. - **Path:** `mfoil/mfoil.py` - **Author:** Krzysztof J. Fidkowski - **License:** MIT -- **Source:** +- **Source:** - **Description:** Python-based airfoil analysis code used as a reference implementation during development. @@ -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) +