Latest revision as of 20:54, 22 October 2022

Click here to return back to Fluid Mechanics

G. Kosec, M. Založnik, B. Šarler, H. Combeau; A meshless approach towards solution of macrosegregation phenomena, Computers, materials & continua : CMC, vol. 22, 2011

G. Kosec, M. Depolli, A. Rashkovska, R. Trobec; Super linear speedup in a local parallel meshless solution of thermo-fluid problem, Computers & Structures, vol. 133, 2014

G. Kosec, B. Šarler; Simulation of macrosegregation with mesosegregates in binary metallic casts by a meshless method, Engineering analysis with boundary elements

M. Maksić, V. Djurica, A. Souvent, J. Slak, M. Depolli, G. Kosec; Cooling of overhead power lines due to the natural convection, International journal of electrical power & energy systems, 2019

Intro

The classical de Vahl Davis benchmark test is defined for the natural convection of the air ($\Pr =0.71$) in the square closed cavity (${{\text{A}}_{\text{R}}}=1$). The only physical free parameter of the test remains the thermal Rayleigh number. In the original paper [1] de Vahl Davis tested the problem up to the Rayleigh number ${{10}^{6}}$, however in the latter publications, the results of more intense simulations were presented with the Rayleigh number up to ${{10}^{8}}$. Lage and Bejan [2] showed that the laminar domain of the closed cavity natural convection problem is roughly below $\text{Gr1}{{\text{0}}^{9}}$. It was reported [3, 4] that the natural convection becomes unsteady for $\text{Ra}=2\cdot {{10}^5}$. Here we present a MLSM solution of the case.

\begin{equation} \text{Ra}\text{=}\,\frac{\left| \mathbf{g} \right|{{\beta }_{T}}\left( {{T}_{H}}-{{T}_{C}} \right){{\Omega }_{H}}^{3}{{\rho }^{2}}{{c}_{p}}}{\lambda \mu } \end{equation} \begin{equation} \text{Pr}=\frac{\mu {{c}_{p}}}{\lambda } \end{equation}

[1] de Vahl Davis G. Natural convection of air in a square cavity: a bench mark numerical solution. Int J Numer Meth Fl. 1983;3:249-64.

[2] Lage JL, Bejan A. The Ra-Pr domain of laminar natural convection in an enclosure heated from the side. Numer Heat Transfer. 1991;A19:21-41.

[3] Janssen RJA, Henkes RAWM. Accuracy of finite-volume disretizations for the bifurcating natural-convection flow in a square cavity. Numer Heat Transfer. 1993;B24:191-207.

[4] Nobile E. Simulation of time-dependent flow in cavities with the additive-correction multigrid method, part II: Apllications. Numer Heat Transfer. 1996;B30:341-50.

. Figure 1: Scheme of the de Vahl Davis benchmark test

Code

Full examples can be found under the examples in the code repository.

Explicit ACM method with CBS looks

 1     v2[boundary] = vec_t{0.0, 0.0};
 2     T2[left] = O.T_cold;
 3     T2[right] = O.T_hot;
 4     //Time stepping
 5     for (int step = 0; step <= O.t_steps; ++step) {
 6         for (int i_count = 1; i_count < _MAX_ITER_; ++i_count) {
 7             // Navier Stokes
 8             for (auto c : interior) {
 9                 v2[c] = v1[c] + O.dt * (-1 / O.rho * op.grad(P1, c)
10                                         + O.mu / O.rho * op.lap(v1, c)
11                                         - op.grad(v1, c) * v1[c]
12                                         + O.g * (1 - O.beta * (T1[c] - O.T_ref)));
13             }
14 
15             //Speed of sound
16             Range<scal_t> norm = v2.map([](const vec_t& p) { return p.norm(); });
17             scal_t C = O.dl * std::max(*std::max_element(norm.begin(), norm.end()), O.v_ref);
18             // Mass continuity
19             Range<scal_t> div_v;
20             for (auto c:all) {
21                 div_v[c] = op.div(v2, c);
22                 P2[c] = P1[c] - C * C * O.dt * O.rho * div_v[c] +
23                         O.dl2 * C * C * O.dt * O.dt * op.lap(P1, c);
24             }
25             P1.swap(P2);
26         }
27 
28         //heat transport
29         for (auto c : interior) {
30             T2[c] = T1[c] + O.dt * O.lam / O.rho / O.c_p * op.lap(T1, c) -
31                     O.dt * v1[c].transpose() * op.grad(T1, c);
32         }
33         for (auto c : top) T2[c] = op.neumann(T2, c, vec_t{0, -1}, 0.0);
34         for (auto c : bottom) T2[c] = op.neumann(T2, c, vec_t{0, 1}, 0.0);
35     }

Explicit pressure correction

The solution of heat equation is the same as in above example

 1     for (int step = 0; step <= O.t_steps; ++step) {
 2         // Explicit Navier-Stokes computed on whole domain, including boundaries
 3         // without pressure
 4         for (int c:all) {
 5             v_2[c] = v_1[c] + O.dt (
 6                                    O.mu / O.rho * op.lap(v_1, c)
 7                                     - op.grad(v_1, c) * v_1[c]
 8                                     + O.g * (1 - O.beta * (T_1[c] - O.T_ref)));
 9         }
10         // Pressure correction
11         VecXd rhs_pressure(N + 1, 0); //Note N+1, +1 stands for regularization equation
12         rhs_pressure(N) = 0; // = 0 part of the regularization equation
13         for (int i:interior) rhs_pressure(c) = O.rho / O.dt * op.div(v_2, c);
14         for (int i: boundary) rhs_pressure(c) = O.rho / O.dt * v_2[c].dot(domain.normal(c));
15         VecXd solution = solver_p.solve(rhs_pressure);
16         alpha = solution[N];
17         VecXd P_c = solution.head(N);
18         for ( int i = interior) v_2[c] -=  O.dt / O.rho * op.grad(P_c, c);
19         v_2[boundary] = 0; // force boundary conditions
20         //heat transport
21         for (auto c : interior) {
22             T2[c] = T1[c] + O.dt * O.lam / O.rho / O.c_p * op.lap(T1, c) -
23                     O.dt * v1[c].transpose() * op.grad(T1, c);
24         }
25         for (auto c : top) T2[c] = op.neumann(T2, c, vec_t{0, -1}, 0.0);
26         for (auto c : bottom) T2[c] = op.neumann(T2, c, vec_t{0, 1}, 0.0);
27 }

Implicit

 1 for (int step = 0; step <= O.t_steps_i; ++step) {
 2         time_1 = std::chrono::high_resolution_clock::now();
 3         // NAVIER STOKES
 4         M_velocity = mat_t(2 * N, 2 * N);
 5         // system
 6         M_velocity.reserve(Range<int>(2 * N, O.n));
 7         for (int i : interior) {
 8             op.valuevec(M_velocity, i, 1 / O.dt_i);
 9             op.lapvec(M_velocity, i, -O.mu / O.rho);
10             op.gradvec(M_velocity, i, v_1[i]);
11         }
12         for (int i : boundary) op.valuevec(M_velocity, i, 1); //sets velocity to 0
13 
14         M_velocity.makeCompressed();
15         solver_v.compute(M_velocity);
16         // solution
17         Range <vec_t> rhs_vec(domain.size(), 0);
18         for (int i : interior) {
19             rhs_vec[i] = -1 / O.rho * op.grad(P, i) +
20                          v_1[i] / O.dt_i
21                          + O.g * (1 - O.beta * (T[i] - O.T_ref));
22         }
23         // for (int i:top) rhs_vec[i] = vec_t{0,1};
24 
25         v_2 = reshape<2>(solver_v.solveWithGuess(reshape(rhs_vec), reshape(v_1)));
26         // END OF NAVIER STOKES
27 
28         // PRESSURE CORRECTION
29         VecXd rhs_pressure(N + 1, 0); //Note N+1, +1 stands for regularization equation
30         rhs_pressure(N) = 0; // = 0 part of the regularization equation
31         double alpha;
32         for (int i : interior) rhs_pressure(i) = O.rho / O.dt_i * op.div(v_2, i);
33         for (int i : boundary) rhs_pressure(i) = O.rho / O.dt * v_2[i].dot(domain.normal(i));
34 
35         VecXd solution = solver_p.solve(rhs_pressure);
36         alpha = solution[N];
37         VecXd P_c = solution.head(N);
38         // apply velocity correction
39         for (int i : interior) {
40             v_2[i] -= O.dl * O.dt_i / O.rho * op.grad(P_c, i);
41         }
42         P += O.dl * P_c;
43         // enforce velocity BC
44         // v_2[boundary] = 0;
45         // END OF PRESSURE CORRECTION
46 
47         // HEAT TRANSPORT
48         M_temperature = mat_t(N, N);
49         Range<int> per_row(N, O.n);
50         M_temperature.reserve(per_row);
51         // outer boundary dirichlet BC
52         for (int i : top) op.neumann_implicit(M_temperature, i, domain.normal(i), 1);
53         for (int i : bottom) op.neumann_implicit(M_temperature, i, domain.normal(i), 1);
54         for (int i : left) op.value(M_temperature, i, 1.0);
55         for (int i : right) op.value(M_temperature, i, 1.0);
56         // heat transport in air
57         for (int i : interior) {
58             op.value(M_temperature, i, 1.0);                          // time dependency
59             op.lap(M_temperature, i, -O.dt_i * O.lam / O.rho / O.c_p);  //laplace in interior
60             op.grad(M_temperature, i, O.dt * v_2[i]);
61         }
62         M_temperature.makeCompressed();
63         solver_T.compute(M_temperature);
64 
65         VectorXd rhs = VectorXd::Zero(N);
66         for (int i : interior) rhs(i) = T(i);
67         for (int i : top) rhs(i) = 0;
68         for (int i : bottom) rhs(i) = 0;
69         for (int i : left) rhs(i) = O.T_hot;
70         for (int i : right) rhs(i) = O.T_cold;
71         T = solver_T.solveWithGuess(rhs, T);
72         // END OF HEAT TRANSPORT
73         v_1.swap(v_2);
74 }

Results

Comparison of MLSM solution with reference data

Following video shows evolution of temperature and velocity magnitude for the $Ra=10^8$ case.

In below galley you can find temperature contour plots, velocity magnitude contour plots, v_max and average hot side Nusselt number convergence behavior. The reference values are from:

[a] de Vahl Davis G. Natural convection of air in a square cavity: a bench mark numerical solution. Int J Numer Meth Fl. 1983;3:249-64.
[b] Sadat H, Couturier S. Performance and accuracy of a meshless method for laminar natural convection. Numer Heat Transfer. 2000;B37:455-67.
[c] Wan DC, Patnaik BSV, Wei GW. A new benchmark quality solution for the buoyancy-driven cavity by discrete singular convolution. Numer Heat Transfer. 2001;B40:199-228.
[d] Šarler B. A radial basis function collocation approach in computational fluid dynamics. CMES-Comp Model Eng. 2005;7:185-93.
[e] Kosec G, Šarler B. Solution of thermo-fluid problems by collocation with local pressure correction. Int J Numer Method H. 2008;18:868-82.

Difference between revisions of "De Vahl Davis natural convection test"

Latest revision as of 20:54, 22 October 2022

Related papers

Intro

Code

Explicit ACM method with CBS looks

Explicit pressure correction

Implicit

Results

Comparison of MLSM solution with reference data

Navigation menu

Personal tools

Namespaces

Variants

Views

More

Search

Navigation

Tools

@@ Line 1: / Line 1: @@
 Click here to return back to [[Fluid Mechanics]]
+{{Box-round|title= Related papers |
+[https://e6.ijs.si/ParallelAndDistributedSystems/publications/992507.pdf G. Kosec, B. Šarler; Solution of thermo-fluid problems by collocation with local pressure correction, International journal of numerical methods for heat & fluid flow, vol.18, 2008]
+[https://e6.ijs.si/ParallelAndDistributedSystems/publications/1905659.pdf G. Kosec, M. Založnik, B. Šarler, H. Combeau; A meshless approach towards solution of macrosegregation phenomena, Computers, materials & continua : CMC, vol. 22, 2011 ]
+[http://comms.ijs.si/~gkosec/data/papers/27339815.pdf G. Kosec, M. Depolli, A. Rashkovska, R. Trobec; Super linear speedup in a local parallel meshless solution of thermo-fluid problem, Computers & Structures, vol. 133, 2014]
+[https://e6.ijs.si/ParallelAndDistributedSystems/publications/3218939.pdf G. Kosec, B. Šarler; Simulation of macrosegregation with mesosegregates in binary metallic casts by a meshless method, Engineering analysis with boundary elements]
+[https://e6.ijs.si/ParallelAndDistributedSystems/publications/32388135.pdf M. Maksić, V. Djurica, A. Souvent, J. Slak, M. Depolli, G. Kosec; Cooling of overhead power lines due to the natural convection, International journal of electrical power & energy systems, 2019]
+}}
 =Intro=
@@ Line 25: / Line 37: @@
 =Code=
-The snippet of the openMP parallel MLSM code for an '''explicit ACM method with CBS looks''' like: (full examples can be found under the examples in the code repository [[Main Page]]).
+Full examples can be found under the examples in the [https://gitlab.com/e62Lab/medusa code repository].
+==Explicit ACM method with CBS looks==
 <syntaxhighlight lang="c++" line>
      v2[boundary] = vec_t{0.0, 0.0};
@@ Line 65: / Line 78: @@
 </syntaxhighlight>
-Snippet of code for explicit pressure correction with fraction step scheme. Note that the solution of heat equation is the same as in above example
+== Explicit pressure correction ==
+The solution of heat equation is the same as in above example
 <syntaxhighlight lang="c++" line>
      for (int step = 0; step <= O.t_steps; ++step) {
          // Explicit Navier-Stokes computed on whole domain, including boundaries
-         // without pressure -- Fraction step
+         // without pressure
          for (int c:all) {
              v_2[c] = v_1[c] + O.dt (
@@ Line 82: / Line 94: @@
          rhs_pressure(N) = 0; // = 0 part of the regularization equation
          for (int i:interior) rhs_pressure(c) = O.rho / O.dt * op.div(v_2, c);
          for (int i: boundary) rhs_pressure(c) = O.rho / O.dt * v_2[c].dot(domain.normal(c));
          VecXd solution = solver_p.solve(rhs_pressure);
          alpha = solution[N];
          VecXd P_c = solution.head(N);
          for ( int i = interior) v_2[c] -=  O.dt / O.rho * op.grad(P_c, c);
          v_2[boundary] = 0; // force boundary conditions
+        //heat transport
+        for (auto c : interior) {
+            T2[c] = T1[c] + O.dt * O.lam / O.rho / O.c_p * op.lap(T1, c) -
+                    O.dt * v1[c].transpose() * op.grad(T1, c);
+        }
+        for (auto c : top) T2[c] = op.neumann(T2, c, vec_t{0, -1}, 0.0);
+        for (auto c : bottom) T2[c] = op.neumann(T2, c, vec_t{0, 1}, 0.0);
+}
+</syntaxhighlight>
+== Implicit ==
+<syntaxhighlight lang="c++" line>
+for (int step = 0; step <= O.t_steps_i; ++step) {
+        time_1 = std::chrono::high_resolution_clock::now();
+        // NAVIER STOKES
+        M_velocity = mat_t(2 * N, 2 * N);
+        // system
+        M_velocity.reserve(Range<int>(2 * N, O.n));
+        for (int i : interior) {
+            op.valuevec(M_velocity, i, 1 / O.dt_i);
+            op.lapvec(M_velocity, i, -O.mu / O.rho);
+            op.gradvec(M_velocity, i, v_1[i]);
+        }
+        for (int i : boundary) op.valuevec(M_velocity, i, 1); //sets velocity to 0
+        M_velocity.makeCompressed();
+        solver_v.compute(M_velocity);
+        // solution
+        Range <vec_t> rhs_vec(domain.size(), 0);
+        for (int i : interior) {
+            rhs_vec[i] = -1 / O.rho * op.grad(P, i) +
+                         v_1[i] / O.dt_i
+                         + O.g * (1 - O.beta * (T[i] - O.T_ref));
+        }
+        // for (int i:top) rhs_vec[i] = vec_t{0,1};
+        v_2 = reshape<2>(solver_v.solveWithGuess(reshape(rhs_vec), reshape(v_1)));
+        // END OF NAVIER STOKES
+        // PRESSURE CORRECTION
+        VecXd rhs_pressure(N + 1, 0); //Note N+1, +1 stands for regularization equation
+        rhs_pressure(N) = 0; // = 0 part of the regularization equation
+        double alpha;
+        for (int i : interior) rhs_pressure(i) = O.rho / O.dt_i * op.div(v_2, i);
+        for (int i : boundary) rhs_pressure(i) = O.rho / O.dt * v_2[i].dot(domain.normal(i));
+        VecXd solution = solver_p.solve(rhs_pressure);
+        alpha = solution[N];
+        VecXd P_c = solution.head(N);
+        // apply velocity correction
+        for (int i : interior) {
+            v_2[i] -= O.dl * O.dt_i / O.rho * op.grad(P_c, i);
+        }
+        P += O.dl * P_c;
+        // enforce velocity BC
+        // v_2[boundary] = 0;
+        // END OF PRESSURE CORRECTION
+        // HEAT TRANSPORT
+        M_temperature = mat_t(N, N);
+        Range<int> per_row(N, O.n);
+        M_temperature.reserve(per_row);
+        // outer boundary dirichlet BC
+        for (int i : top) op.neumann_implicit(M_temperature, i, domain.normal(i), 1);
+        for (int i : bottom) op.neumann_implicit(M_temperature, i, domain.normal(i), 1);
+        for (int i : left) op.value(M_temperature, i, 1.0);
+        for (int i : right) op.value(M_temperature, i, 1.0);
+        // heat transport in air
+        for (int i : interior) {
+            op.value(M_temperature, i, 1.0);                          // time dependency
+            op.lap(M_temperature, i, -O.dt_i * O.lam / O.rho / O.c_p);  //laplace in interior
+            op.grad(M_temperature, i, O.dt * v_2[i]);
+        }
+        M_temperature.makeCompressed();
+        solver_T.compute(M_temperature);
+        VectorXd rhs = VectorXd::Zero(N);
+        for (int i : interior) rhs(i) = T(i);
+        for (int i : top) rhs(i) = 0;
+        for (int i : bottom) rhs(i) = 0;
+        for (int i : left) rhs(i) = O.T_hot;
+        for (int i : right) rhs(i) = O.T_cold;
+        T = solver_T.solveWithGuess(rhs, T);
+        // END OF HEAT TRANSPORT
+        v_1.swap(v_2);
+}
 </syntaxhighlight>
 =Results=
+== Comparison of MLSM solution with reference data  ==
 Following video shows evolution of temperature and velocity magnitude for the $Ra=10^8$ case.