use symmetrisation from [0]
[0]: Two-Dimensional Inlet Simulation Using a Diagonal Implicit Algorithm, Chausee & Pulliam, AIAA Journal
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@ -610,14 +610,11 @@ fn upwind_dissipation(
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let mut tmp0 = tmp.0.view_mut().into_shape((4, n)).unwrap();
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let mut tmp1 = tmp.1.view_mut().into_shape((4, n)).unwrap();
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for (
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((((((y, mut tmp0), mut tmp1), detj), detj_dxi_dx), detj_dxi_dy), detj_deta_dx),
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detj_deta_dy,
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) in yview
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for ((((((y, mut tmp0), mut tmp1), detj_dxi_dx), detj_dxi_dy), detj_deta_dx), detj_deta_dy) in
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yview
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.axis_iter(ndarray::Axis(1))
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.zip(tmp0.axis_iter_mut(ndarray::Axis(1)))
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.zip(tmp1.axis_iter_mut(ndarray::Axis(1)))
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.zip(metrics.detj().iter())
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.zip(metrics.detj_dxi_dx().iter())
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.zip(metrics.detj_dxi_dy().iter())
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.zip(metrics.detj_deta_dx().iter())
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@ -632,27 +629,27 @@ fn upwind_dissipation(
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let u = rhou / rho;
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let v = rhov / rho;
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let uhat = detj_dxi_dx / detj * u + detj_dxi_dy / detj * v;
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let vhat = detj_deta_dx / detj * u + detj_deta_dy / detj * v;
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let uhat = detj_dxi_dx * u + detj_dxi_dy * v;
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let vhat = detj_deta_dx * u + detj_deta_dy * v;
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let p = pressure(GAMMA, rho, rhou, rhov, e);
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assert!(p > 0.0);
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let c = (GAMMA * p / rho).sqrt();
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let alpha_u = uhat.abs() + c;
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let alpha_v = vhat.abs() + c;
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let alpha_u = uhat.abs() + c * Float::hypot(*detj_dxi_dx, *detj_dxi_dy);
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let alpha_v = vhat.abs() + c * Float::hypot(*detj_deta_dx, *detj_deta_dy);
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tmp0[0] = alpha_u * rho * detj;
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tmp1[0] = alpha_v * rho * detj;
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tmp0[0] = alpha_u * rho;
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tmp1[0] = alpha_v * rho;
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tmp0[1] = alpha_u * rhou * detj;
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tmp1[1] = alpha_v * rhou * detj;
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tmp0[1] = alpha_u * rhou;
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tmp1[1] = alpha_v * rhou;
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tmp0[2] = alpha_u * rhov * detj;
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tmp1[2] = alpha_v * rhov * detj;
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tmp0[2] = alpha_u * rhov;
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tmp1[2] = alpha_v * rhov;
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tmp0[3] = alpha_u * e * detj;
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tmp1[3] = alpha_v * e * detj;
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tmp0[3] = alpha_u * e;
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tmp1[3] = alpha_v * e;
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}
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op.dissxi(tmp.0.rho(), k.0.rho_mut());
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@ -1099,15 +1096,16 @@ fn SAT_characteristic(
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let p = pressure(GAMMA, rho, rhou, rhov, e);
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let c = (GAMMA * p / rho).sqrt();
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let phi2 = (GAMMA - 1.0) * (u * u + v * v) / 2.0;
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let alpha = rho / (sbp::consts::SQRT_2 * c);
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let phi2_c2 = (phi2 + c * c) / (GAMMA - 1.0);
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#[rustfmt::skip]
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let T = [
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[ 1.0, 0.0, 1.0, 1.0],
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[ u, ky, u + kx * c, u - kx * c],
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[ v, -kx, v + ky * c, v - ky * c],
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[phi2 / (GAMMA - 1.0), ky * u - kx * v, phi2_c2 + c * theta, phi2_c2 - c * theta],
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[ 1.0, 0.0, alpha, alpha],
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[ u, ky, alpha*(u + kx * c), alpha*(u - kx * c)],
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[ v, -kx, alpha*(v + ky * c), alpha*(v - ky * c)],
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[phi2 / (GAMMA - 1.0), rho*(ky * u - kx * v), alpha*(phi2_c2 + c * theta), alpha*(phi2_c2 - c * theta)],
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];
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let U = kx_ * u + ky_ * v;
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let L = [
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@ -1120,7 +1118,7 @@ fn SAT_characteristic(
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#[rustfmt::skip]
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let TI = [
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[ 1.0 - phi2 / (c * c), (GAMMA - 1.0) * u / (c * c), (GAMMA - 1.0) * v / (c * c), -(GAMMA - 1.0) / (c * c)],
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[ -(ky * u - kx * v), ky, -kx, 0.0],
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[ -(ky * u - kx * v)/rho, ky/rho, -kx/rho, 0.0],
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[beta * (phi2 - c * theta), beta * (kx * c - (GAMMA - 1.0) * u), beta * (ky * c - (GAMMA - 1.0) * v), beta * (GAMMA - 1.0)],
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[beta * (phi2 + c * theta), -beta * (kx * c + (GAMMA - 1.0) * u), -beta * (ky * c + (GAMMA - 1.0) * v), beta * (GAMMA - 1.0)],
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];
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