fix: minor typo in doc
@@ -251,7 +251,7 @@ def get_ielem_inode(connectivities, inode):
def get_aoacl0_from_camber(x, y):
"""
- This section provies the angle of attach of zero lift for a thin
+ This section provies the angle of attack of zero lift for a thin
airfoil which camber line is defined by 'x' and 'y' coordinates
Check Theory of wing sections. Abbott. pg 69
