import numpy as np import matplotlib.pyplot as plt PI = np.pi np.set_printoptions(precision=2, floatmode="maxprec", suppress=True) figure, axes = plt.subplots() cb = None Re = 100 nu = 1 / Re domain_size = (1, 2) step = 0.05 N = int(domain_size[0] / step) M = int(domain_size[1] / step) shape = (N, M) alpha = 1 # Coefficient t_m = 1 h_c = 0.3 l_c = 0.6 # Staggered vars u = np.zeros(shape=shape, dtype=float) u_star = np.zeros(shape=shape, dtype=float) u_new = np.zeros(shape=shape, dtype=float) v = np.zeros(shape=shape, dtype=float) v_star = np.zeros(shape=shape, dtype=float) v_new = np.zeros(shape=shape, dtype=float) p = np.zeros(shape=shape, dtype=float) p_star = np.zeros(shape=shape, dtype=float) p_new = np.zeros(shape=shape, dtype=float) d_e = np.zeros(shape=shape, dtype=float) d_n = np.zeros(shape=shape, dtype=float) b = np.zeros(shape=shape, dtype=float) def u_boundary(t, y): def f(t): return 1 if t_m < t else 0.5 * (np.sin(0.5 * PI * (2 * t / t_m - 1)) + 1) return 6 * f(t) * (y - h_c) * (1 - y) / (1 - h_c)**2 # Loop error = 1 precision = 10 ** -7 t = 0.35 iteration = 0 while error > precision: iteration += 1 # Inflow boundary condition for i in range(N): y = domain_size[0] - i * step u_star[i][0] = u_boundary(t, y) v_star[i][0] = 0 # Sides boundary conditions for j in range(M): v_star[0][j] = 0 v_star[N - 1][j] = 0 u_star[0][j] = 0 u_star[N - 1][j] = 0 # x-momentum for i in range(1, N - 1): for j in range(1, M - 1): u_E = 0.5 * (u[i][j] + u[i][j + 1]) u_W = 0.5 * (u[i][j] + u[i][j - 1]) v_N = 0.5 * (v[i - 1][j] + v[i - 1][j + 1]) v_S = 0.5 * (v[i][j] + v[i][j + 1]) a_E = -0.5 * u_E * step + nu a_W = +0.5 * u_W * step + nu a_N = -0.5 * v_N * step + nu a_S = +0.5 * v_S * step + nu a_e = 0.5 * step * (u_E - u_W + v_N - v_S) + 4 * nu A_e = -step d_e[i][j] = A_e / a_e u_star[i][j] = (a_E * u[i][j + 1] + a_W * u[i][j - 1] + a_N * u[i - 1][j] + a_S * u[i + 1][j]) / a_e + d_e[i][j] * (p[i][j + 1] - p[i][j]) # y-momentum for i in range(1, N - 1): for j in range(1, M - 1): u_E = 0.5 * (u[i][j] + u[i + 1][j]) u_W = 0.5 * (u[i][j - 1] + u[i + 1][j - 1]) v_N = 0.5 * (v[i - 1][j] + v[i][j]) v_S = 0.5 * (v[i][j] + v[i + 1][j]) a_E = -0.5 * u_E * step + nu a_W = +0.5 * u_W * step + nu a_N = -0.5 * v_N * step + nu a_S = +0.5 * v_S * step + nu a_n = 0.5 * step * (u_E - u_W + v_N - v_S) + 4 * nu A_n = -step d_n[i][j] = A_n / a_n v_star[i][j] = (a_E * v[i][j + 1] + a_W * v[i][j - 1] + a_N * v[i - 1][j] + a_S * v[i + 1][j]) / a_n + d_n[i][j] * (p[i][j] - p[i + 1][j]) # Backwards-facing step boundary conditions (same as sides) for i in range(int(h_c / step)): for j in range(int(l_c / step)): u_star[i][j] = 0 v_star[i][j] = 0 p_new[i][j] = 100 # Pressure correction p_c = np.zeros(shape=shape, dtype=float) for i in range(1, N - 1): for j in range(1, M - 1): a_E = -d_e[i][j] * step a_W = -d_e[i][j-1] * step a_N = -d_n[i-1][j] * step a_S = -d_n[i][j] * step a_P = a_E + a_W + a_N + a_S b[i][j] = step * (-(u_star[i][j] - u_star[i][j-1]) + (v_star[i][j] - v_star[i-1][j])) p_c[i][j] = (a_E * p_c[i][j+1] + a_W * p_c[i][j-1] + a_N * p_c[i-1][j] + a_S * p_c[i+1][j] + b[i][j]) / a_P p_new = p + p_c * alpha # Pressure boundaries for i in range(N - 1): p_new[i][0] = p_new[i][1] p_new[i][M - 1] = p_new[i][M - 2] for j in range(M - 1): p_new[0][j] = p_new[1][j] p_new[N - 1][j] = p_new[N - 2][j] # Velocity correction for i in range(1, N - 1): for j in range(1, M - 1): u_new[i][j] = u_star[i][j] + alpha * d_e[i][j] * (p_c[i + 1][j] - p_c[i][j]) v_new[i][j] = v_star[i][j] + alpha * d_n[i][j] * (p_c[i][j] - p_c[i + 1][j]) # Continuity residual as error measure error = 0 for i in range(N): for j in range(M): error += abs(b[i][j]) u = u_new v = v_new p = p_new # Plotting print(error) x, y = np.meshgrid( np.linspace(0, domain_size[1], shape[1]), np.linspace(0, domain_size[0], shape[0]), ) if iteration % 100 == 0: pcolormesh = axes.pcolormesh(x, y, p, cmap='PuBuGn') if (cb): cb.remove() cb = plt.colorbar(pcolormesh) factor = np.sqrt(u ** 2 + v ** 2) u_normalized = u / factor v_normalized = v / factor plt.quiver(x, y, u_normalized, v_normalized, scale=30) plt.pause(0.0001) plt.show()