pymead.analysis.calc_aero_data.compute_alpha_zero_lift#
- compute_alpha_zero_lift(alpha_deg: ndarray, Cl: ndarray, linear_eps: float = 0.001) float[source]#
Computes the zero-lift angle of attack for an input set of angles of attack and lift coefficients. If no linear regime is detected,
Noneis returned.- Parameters:
alpha_deg (numpy.ndarray) – One-dimensional array of angle of attack in degrees.
Cl (numpy.ndarray) – One-dimensional array of lift coefficients, one-to-one mapping with
alpha_deglinear_eps (float) – Tolerance used to determine whether a linear regime is present in the range of angles of attack provided as input. Default:
0.001
- Returns:
The zero-lift angle of attack in degrees if the linear regime is detected, otherwise
None- Return type:
float or None