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Commit 933aa489 authored by Tamburrini Robin's avatar Tamburrini Robin
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fix: Reynolds below 200000 created issues

parent 5091eea2
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src/airfoil_data/calc_polar.py
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......@@ -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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