1 all[] all[] INLET OUTLET STAND GROUND TOP FRONT BACK 2.125 1.6 0.865 2.125 1.6 1.1 2.24 1.6 1.15 2.355 1.6 1.1 2.355 1.6 0.865 2.5 1.495 0.9825 2.3 1.6 0.5 2.4 1.6 0.5 2.5 1.6 0.5 2.6 1.6 0.5 2.7 1.6 0.5 2.3 1.6 0.9825 2.4 1.6 0.9825 2.5 1.6 0.9825 2.6 1.6 0.9825 2.7 1.6 0.9825 2.3 1.6 0.865 2.4 1.6 0.865 2.5 1.6 0.865 2.6 1.6 0.865 2.7 1.6 0.865 2.3 1.6 1.1 2.4 1.6 1.1 2.5 1.6 1.1 2.6 1.6 1.1 2.7 1.6 1.1 2.3 1.6 0.2 2.4 1.6 0.2 2.5 1.6 0.2 2.6 1.6 0.2 2.7 1.6 0.2 1 1.0 0.5

# parameter s in [0,1] x0 = 0.01; x1 = 0.01; y0 = 1.6; y1 = 1.6; z0 = 0.0; z1 = 2.8; x = x1*s + x0*(1.-s); y = y1*s + y0*(1.-s); z = z1*s + z0*(1.-s); yes 1 time_value 1000 # parameter s in [0,1] x0 = 1.8; x1 = 1.8; y0 = 1.6; y1 = 1.6; z0 = 0.0; z1 = 2.8; x = x1*s + x0*(1.-s); y = y1*s + y0*(1.-s); z = z1*s + z0*(1.-s); yes 1 time_value 1000 0.2 -1 0.2 -1 0.2 -1 0.2 -1 0.2 -1 0.2 -1 0.2 -1 0.2 -1 0.2 -1 0.2 -1 0.2 -1 0.2 -1 6 0 1e-06 INLET OUTLET GROUND TOP FRONT BACK STAND kappa = 0.41; Cmu = 0.09; C1 = 0.0; C2 = 1.0; z0 = 0.02; zref2 = 10.0; uref2 = Vref; u_star2 = uref2 * kappa / log((zref2 + z0) / z0); k = (u_star2 ^ 2) / sqrt(Cmu) * sqrt(C1 * log((z + z0) / z0) + C2); omega = u_star2 / (kappa * sqrt(Cmu) * (z + z0)); 2.8 10 0 0 0 kappa = 0.41; Cmu = 0.09; C1 = 0.0; C2 = 1.0; z0 = 0.02; zref2 = 10.0; uref2 = Vref; u_star2 = uref2 * kappa / log((zref2 + z0) / z0); u_norm = (u_star2 / kappa) * log((z + z0) / z0); 0 0 0 0 0 0 0 1.17862 1.83e-05 101325 293.15 0 0 0 0 0 0 all[] 1.0 off 67 0 1 1e-06 0 1 1e-06 3 kappa = 0.41; Cmu = 0.09; C1 = 0.0; C2 = 1.0; z0 = 0.02; zref2 = 10.0; uref2 = Vref; u_star2 = uref2 * kappa / log((zref2 + z0) / z0); u_norm = (u_star2 / kappa) * log((z + z0) / z0); velocity[0]=u_norm; velocity[1] = 0.; velocity[2] = 0.; 2 1e-06 1 1 1e-06