Source code for aerosandbox.aerodynamics.aero_3D.singularities.uniform_strength_horseshoe_singularities

import aerosandbox.numpy as np
from typing import Union


[docs]def calculate_induced_velocity_horseshoe( x_field: Union[float, np.ndarray], y_field: Union[float, np.ndarray], z_field: Union[float, np.ndarray], x_left: Union[float, np.ndarray], y_left: Union[float, np.ndarray], z_left: Union[float, np.ndarray], x_right: Union[float, np.ndarray], y_right: Union[float, np.ndarray], z_right: Union[float, np.ndarray], gamma: Union[float, np.ndarray] = 1, trailing_vortex_direction: np.ndarray = None, vortex_core_radius: float = 0, ) -> [Union[float, np.ndarray], Union[float, np.ndarray], Union[float, np.ndarray]]: """ Calculates the induced velocity at a point: [x_field, y_field, z_field] in a 3D potential-flow flowfield. In this flowfield, the following singularity elements are assumed: * A single horseshoe vortex consisting of a bound leg and two trailing legs This function consists entirely of scalar, elementwise NumPy ufunc operations - so it can be vectorized as desired assuming input dimensions/broadcasting are compatible. Args: x_field: x-coordinate of the field point y_field: y-coordinate of the field point z_field: z-coordinate of the field point x_left: x-coordinate of the left vertex of the bound vortex y_left: y-coordinate of the left vertex of the bound vortex z_left: z-coordinate of the left vertex of the bound vortex x_right: x-coordinate of the right vertex of the bound vortex y_right: y-coordinate of the right vertex of the bound vortex z_right: z-coordinate of the right vertex of the bound vortex gamma: The strength of the horseshoe vortex filament. trailing_vortex_direction: The direction that the trailing legs of the horseshoe vortex extend. Usually, this is modeled as the direction of the freestream. vortex_core_radius: To prevent a vortex singularity, here we use a Kaufmann vortex model. This parameter governs the radius of this vortex model. It should be significantly smaller (e.g., at least an order of magnitude smaller) than the smallest bound leg in the analysis in question. Returns: u, v, and w: The x-, y-, and z-direction induced velocities. """ if trailing_vortex_direction is None: trailing_vortex_direction = np.array([1, 0, 0]) np.assert_equal_shape({ "x_field": x_field, "y_field": y_field, "z_field": z_field, }) np.assert_equal_shape({ "x_left" : x_left, "y_left" : y_left, "z_left" : z_left, "x_right": x_right, "y_right": y_right, "z_right": z_right, }) a_x = np.add(x_field, -x_left) a_y = np.add(y_field, -y_left) a_z = np.add(z_field, -z_left) b_x = np.add(x_field, -x_right) b_y = np.add(y_field, -y_right) b_z = np.add(z_field, -z_right) u_x = trailing_vortex_direction[0] u_y = trailing_vortex_direction[1] u_z = trailing_vortex_direction[2] # Handle the special case where the field point is on one of the legs (either bound or trailing) def smoothed_inv(x): "Approximates 1/x with a function that sharply goes to 0 in the x -> 0 limit." if not np.all(vortex_core_radius == 0): return x / (x ** 2 + vortex_core_radius ** 2) else: return 1 / x ### Do some useful arithmetic a_cross_b_x = a_y * b_z - a_z * b_y a_cross_b_y = a_z * b_x - a_x * b_z a_cross_b_z = a_x * b_y - a_y * b_x a_dot_b = a_x * b_x + a_y * b_y + a_z * b_z a_cross_u_x = a_y * u_z - a_z * u_y a_cross_u_y = a_z * u_x - a_x * u_z a_cross_u_z = a_x * u_y - a_y * u_x a_dot_u = a_x * u_x + a_y * u_y + a_z * u_z b_cross_u_x = b_y * u_z - b_z * u_y b_cross_u_y = b_z * u_x - b_x * u_z b_cross_u_z = b_x * u_y - b_y * u_x b_dot_u = b_x * u_x + b_y * u_y + b_z * u_z norm_a = (a_x ** 2 + a_y ** 2 + a_z ** 2) ** 0.5 norm_b = (b_x ** 2 + b_y ** 2 + b_z ** 2) ** 0.5 norm_a_inv = smoothed_inv(norm_a) norm_b_inv = smoothed_inv(norm_b) ### Calculate Vij term1 = (norm_a_inv + norm_b_inv) * smoothed_inv(norm_a * norm_b + a_dot_b) term2 = norm_a_inv * smoothed_inv(norm_a - a_dot_u) term3 = norm_b_inv * smoothed_inv(norm_b - b_dot_u) constant = gamma / (4 * np.pi) u = np.multiply( constant, ( a_cross_b_x * term1 + a_cross_u_x * term2 - b_cross_u_x * term3 ) ) v = np.multiply( constant, ( a_cross_b_y * term1 + a_cross_u_y * term2 - b_cross_u_y * term3 ) ) w = np.multiply( constant, ( a_cross_b_z * term1 + a_cross_u_z * term2 - b_cross_u_z * term3 ) ) return u, v, w
if __name__ == '__main__': ##### Check single vortex u, v, w = calculate_induced_velocity_horseshoe( x_field=0, y_field=0, z_field=0, x_left=-1, y_left=-1, z_left=0, x_right=-1, y_right=1, z_right=0, gamma=1, ) print(u, v, w) ##### Plot grid of single vortex
[docs] args = (-2, 2, 30)
x = np.linspace(*args) y = np.linspace(*args) z = np.linspace(*args) X, Y, Z = np.meshgrid(x, y, z) Xf = X.flatten() Yf = Y.flatten() Zf = Z.flatten() left = [0, -1, 0] right = [0, 1, 0] Uf, Vf, Wf = calculate_induced_velocity_horseshoe( x_field=Xf, y_field=Yf, z_field=Zf, x_left=left[0], y_left=left[1], z_left=left[2], x_right=right[0], y_right=right[1], z_right=right[2], gamma=1, ) pos = np.stack((Xf, Yf, Zf)).T dir = np.stack((Uf, Vf, Wf)).T dir_norm = np.reshape(np.linalg.norm(dir, axis=1), (-1, 1)) dir = dir / dir_norm * dir_norm ** 0.2 import pyvista as pv pv.set_plot_theme('dark') plotter = pv.Plotter() plotter.add_arrows( cent=pos, direction=dir, mag=0.15 ) plotter.add_lines( lines=np.array([ [Xf.max(), left[1], left[2]], left, right, [Xf.max(), right[1], right[2]] ]) ) plotter.show_grid() plotter.show() ##### Check multiple vortices args = (-2, 2, 30) x = np.linspace(*args) y = np.linspace(*args) z = np.linspace(*args) X, Y, Z = np.meshgrid(x, y, z) Xf = X.flatten() Yf = Y.flatten() Zf = Z.flatten() left = [0, -1, 0] center = [0, 0, 0] right = [0, 1, 0] lefts = np.array([left, center]) rights = np.array([center, right]) strengths = np.array([2, 1]) def wide(array): return np.reshape(array, (1, -1)) def tall(array): return np.reshape(array, (-1, 1)) Uf_each, Vf_each, Wf_each = calculate_induced_velocity_horseshoe( x_field=wide(Xf), y_field=wide(Yf), z_field=wide(Zf), x_left=tall(lefts[:, 0]), y_left=tall(lefts[:, 1]), z_left=tall(lefts[:, 2]), x_right=tall(rights[:, 0]), y_right=tall(rights[:, 1]), z_right=tall(rights[:, 2]), gamma=tall(strengths), ) Uf = np.sum(Uf_each, axis=0) Vf = np.sum(Vf_each, axis=0) Wf = np.sum(Wf_each, axis=0) pos = np.stack((Xf, Yf, Zf)).T dir = np.stack((Uf, Vf, Wf)).T dir_norm = np.reshape(np.linalg.norm(dir, axis=1), (-1, 1)) dir = dir / dir_norm * dir_norm ** 0.2 import pyvista as pv pv.set_plot_theme('dark') plotter = pv.Plotter() plotter.add_arrows( cent=pos, direction=dir, mag=0.15 ) plotter.add_lines( lines=np.array([ [Xf.max(), left[1], left[2]], left, center, [Xf.max(), center[1], center[2]], center, right, [Xf.max(), right[1], right[2]] ]) ) plotter.show_grid() plotter.show()