pfh.glidersim.extras.compute_polars#

Utility functions for analyzing wing performance.

Functions

`compute_polar_data`(glider[, rho_air, N])	Compute the equilibrium conditions over the range of control inputs.
`plot_wing_coefficients`(wing[, delta_b, ...])

pfh.glidersim.extras.compute_polars.compute_polar_data(glider, rho_air: float = 1.225, N: int = 21)#: Compute the equilibrium conditions over the range of control inputs.

pfh.glidersim.extras.compute_polars.plot_wing_coefficients(wing, delta_b: float = 0, v_mag: float = 10, rho_air: float = 1.225) → None#