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4 changes: 2 additions & 2 deletions src/xfoil/xfoil.py
Original file line number Diff line number Diff line change
Expand Up @@ -252,7 +252,7 @@ def aseq(self, a_start, a_end, a_step):

Returns
-------
a, cl, cd, cm, co : np.ndarray
a, cl, cd, cm, cp : np.ndarray
Lists of angles of attack and their corresponding lift, drag, moment, and minimum pressure coefficients.
"""
n = abs(int((a_end - a_start) / a_step))
Expand Down Expand Up @@ -289,7 +289,7 @@ def cseq(self, cl_start, cl_end, cl_step):

Returns
-------
a, cl, cd, cm, co : np.ndarray
a, cl, cd, cm, cp : np.ndarray
Lists of angles of attack and their corresponding lift, drag, moment, and minimum pressure coefficients.
"""
n = abs(int((cl_end - cl_start) / cl_step))
Expand Down