From 933aa4892a7fcc2242cbb79adc22a0bc8e232c94 Mon Sep 17 00:00:00 2001
From: Robin Tamburrini <robin.tamburrini@student.uliege.be>
Date: Fri, 1 Mar 2024 09:44:56 +0100
Subject: [PATCH] fix: Reynolds below 200000 created issues

---
 src/airfoil_data/calc_polar.py | 4 ++--
 1 file changed, 2 insertions(+), 2 deletions(-)

diff --git a/src/airfoil_data/calc_polar.py b/src/airfoil_data/calc_polar.py
index 2b985e0..2ff80cb 100644
--- a/src/airfoil_data/calc_polar.py
+++ b/src/airfoil_data/calc_polar.py
@@ -3,8 +3,8 @@
 import numpy as np
 from xfoil import calc_polar
 
-NACA = "0021"
-REYNOLDS = [re * 1000000 for re in [0.02, 0.1, 0.2, 0.5, 1, 2, 5, 10]]
+NACA = "0030"
+REYNOLDS = [re * 1000000 for re in [0.2, 0.5, 1, 2, 5, 10]]
 
 
 for re in REYNOLDS:
-- 
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