% Axisymmetric mug % r–z plane, rotation around r = 0 clear; clc; close all; %% General values that we use in the entire script maxIter = 5000; tol = 1e-6; %Task 3) Thermal conductivity lambda_wall = 2.0; % ceramic RANDOM NUMBER lambda_fluid = 0.6; % water RANDOM NUMBER lambda_air = 0.025; % air RANDOM NUMBER %Task 4) alpha = 10; % heat transfer coefficient u_out = 18; % ambient air temperature (°C) %Task 6) Heat capacities (example values) c_wall = 900; % ceramic RANDOM NUMBER c_fluid = 4180; % water RANDOM NUMBER c_air = 1005; % air RANDOM NUMBER % This numbers don't simulate real life because in real life we have % volumetric heat capacities. this means we are having a reduced factore of % approx 10^4. %% Task 1: Mesh definition % Create PDE model model = createpde(); % Points (meters) A = [0, 0]; B = [0.055, 0]; C = [0.083, 0.105]; H = [0.078, 0.105]; F = [0.050, 0.005]; E = [0, 0.005]; G = [0.067, 0.066]; I = [0, 0.066]; D = [0, 0.105]; % Geometry matrix (edges) % Axis (split by material) g1 = [2; A(1); E(1); A(2); E(2); 1; 0]; % ceramic g2 = [2; E(1); I(1); E(2); I(2); 2; 0]; % fluid g3 = [2; I(1); D(1); I(2); D(2); 3; 0]; % air % Outer ceramic g4 = [2; A(1); B(1); A(2); B(2); 1; 0]; g5 = [2; B(1); C(1); B(2); C(2); 1; 0]; % Top rim: C -> H is ceramic-air (ONLY) g6 = [2; C(1); H(1); C(2); H(2); 1; 3]; % Inner ceramic wall (H -> F) ceramic-air g7 = [2; H(1); F(1); H(2); F(2); 1; 3]; % Inner ceramic bottom (F -> E) ceramic-fluid g8 = [2; F(1); E(1); F(2); E(2); 1; 2]; % Fluid surface (F -> G) fluid-air g9 = [2; F(1); G(1); F(2); G(2); 2; 3]; % Fluid surface (G -> I) fluid-air g10 = [2; G(1); I(1); G(2); I(2); 2; 3]; % Air top boundary: D -> H (air-outside) g11 = [2; D(1); H(1); D(2); H(2); 3; 0]; % Assemble geometry g = [g1 g2 g3 g4 g5 g6 g7 g8 g9 g10 g11]; % Load geometry into PDE model geometryFromEdges(model, g); % Plot geometry with labels % figure(1); % pdegplot(model, 'EdgeLabels','on', 'FaceLabels','on'); % axis equal; % title('Geometry with edge and face labels'); % Generate mesh mesh = generateMesh(model, 'Hmax', 0.006, 'GeometricOrder','linear'); % Plot mesh % figure(2); % pdemesh(model); % axis equal; % title('Generated mesh'); %% Task 2: Jacobi solver with constant lambda nodes = mesh.Nodes; % coordinates of all mesh nodes elements = mesh.Elements; % which nodes make up each triangle element Nnodes = size(nodes,2); Nelems = size(elements,2); % Define material properties (for simplicity, lambda = 1 everywhere) lambda = ones(Nelems,1); % thermal conductivity % Initialize global stiffness matrix and RHS K = sparse(Nnodes, Nnodes); F = zeros(Nnodes,1); % Assemble K and F for e = 1:Nelems %Loop over each triangle element vert = elements(:,e); %nodes of element x = nodes(1,vert); y = nodes(2,vert); Ae = polyarea(x,y); % Compute area of the triangle % Linear triangle gradients b = [y(2)-y(3); y(3)-y(1); y(1)-y(2)]; % derivative with respect to x c = [x(3)-x(2); x(1)-x(3); x(2)-x(1)]; % derivative with respect to y % Element stiffness matrix Ke = (lambda(e)/(4*Ae)) * (b*b.' + c*c.'); % Assemble K(vert,vert) = K(vert,vert) + Ke; % Element load vector (f=0) F(vert) = F(vert) + zeros(3,1); end % Find boundary nodes (couldn't find a better way) edgesAll = [elements([1 2],:), elements([2 3],:), elements([3 1],:)]; % all edges -> 2x(3*Nelems) awway since each triangle has 3 edges edgesSorted = sort(edgesAll,1); % sort nodes of each edge, ensure that [i,j] and [j,i] are the same [~,~,ic] = unique(edgesSorted','rows'); % identifies unique edges and assignes indices ic counts = accumarray(ic,1); % counts how many times each edge appears in the mesh boundaryEdges = find(counts==1); %edges belonging to only 1 element: hence on the boundary boundaryNodes = unique(edgesSorted(:,boundaryEdges)); % nodes belonging to these boundary edges % Jacobi iteration D = diag(K); R = K - diag(D); u = zeros(Nnodes,1); for iter = 1:maxIter u_new = (F - R*u) ./ D; u_new(boundaryNodes) = 0; % Enforce Dirichlet BC if norm(u_new - u, inf) < tol % Convergence check fprintf('Task 2) Jacobi converged in %d iterations.\n', iter); break; end u = u_new; end % % Plot solution % figure(3) % pdeplot(model, 'XYData', u, 'Mesh','on'); % axis equal; % title('Stationary Dirichlet solution via Jacobi'); % colorbar; %% Task 3: Laplace with multiple lambdas [K, F] = CalculateLaplace_mult(model, lambda_wall, lambda_fluid, lambda_air); D = diag(K); R = K - diag(D); u = zeros(Nnodes,1); for iter = 1:maxIter u_new = (F - R*u) ./ D; u_new(boundaryNodes) = 0; % Dirichlet BC if norm(u_new - u, inf) < tol fprintf('Task 3) Jacobi converged in %d iterations.\n', iter); break; end u = u_new; end % figure(4) % pdeplot(model, 'XYData', u, 'Mesh','on'); % axis equal % title('Task 3: Stationary solution with multiple conductivities'); % colorbar %% Task 4: Robin boundary condition [K, F] = ApplyRobinBC_mult(model, K, F, alpha, u_out); D = diag(K); R = K - diag(D); u = zeros(Nnodes,1); for iter = 1:maxIter u_new = (F - R*u) ./ D; if norm(u_new - u, inf) < tol fprintf('Task 4) Jacobi (Robin BC) converged in %d iterations.\n', iter); break; end u = u_new; end figure(5) pdeplot(model, 'XYData', u, 'Mesh','on'); axis equal title('Task 4: Stationary solution with Robin BC'); colorbar %% Task 5: Axisymmetric Laplace + Robin BC [K, F] = CalculateLaplace_mult_rot(model, lambda_wall, lambda_fluid, lambda_air); [K, F] = ApplyRobinBC_mult_rot(model, K, F, alpha, u_out); D = diag(K); R = K - diag(D); u = zeros(Nnodes,1); for iter = 1:maxIter u_new = (F - R*u) ./ D; if norm(u_new - u, inf) < tol fprintf('Task 5) Jacobi (axisymmetric Robin) converged in %d iterations.\n', iter); break; end u = u_new; end % Plot solution % figure(6) % pdeplot(model, 'XYData', u, 'Mesh','on'); % axis equal % title('Task 5: Axisymmetric stationary solution with Robin BC'); % colorbar %To see it in 3D paste here the code in "AdditionalPlotCodes.txt". %% Task 6: Axisymmetric mass matrix M = sparse(Nnodes, Nnodes); M = AddMass_mult_rot(model, M, c_wall, c_fluid, c_air); %% Task 7: Initial solution u0 = Init_Solution_mult(model, 18, 80, 18); % figure(7) % pdeplot(model, 'XYData', u0, 'Mesh','on'); % axis equal % title('Initial temperature distribution'); % colorbar %% Task 8: Time-dependent simulation (explicit scheme) tau = 0.5; % time step in seconds T_end = 400; % total simulation time (seconds) Nt = ceil(T_end/tau); % number of time steps A = (1/tau)*M+K; % Left-hand side matrix [L,U,P,Q] = lu(A); % A is constant -> factorize it once: PAQ=LU % Initialize solution u = u0; for k = 1:Nt b = (1/tau)*M*u + F; % F is the load vector, F=0 % Solve for next time step u_next = Q*(U\(L\(P*b))); % efficient solution using LU factors u = u_next; % Update if mod(k,20) == 0 % figure(8) % pdeplot(model, 'XYData', u, 'Mesh','on'); % axis equal % title(['Temperature at t = ', num2str(k*tau), ' s']); % colorbar % drawnow end end %To see the 9 snapshots paste here the codes in "AdditionalPlotCodes.txt" %% Task 9 (i): Heating time using inner ceramic wall temperature T_target = 67; % [°C] innerWallNodes = findNodes(model.Mesh,'region','Edge',8); % Edge 8 = ceramic–fluid interface u = u0; % Storage timeVec = (0:Nt-1)' * tau; innerWallTemp = zeros(Nt,1); Twarm = NaN; for k = 1:Nt b = (1/tau)*M*u + F; u = Q*(U\(L\(P*b))); % Average inner wall temperature innerWallTemp(k) = mean(u(innerWallNodes)); % Check heating criterion if innerWallTemp(k) >= T_target Twarm = k * tau; fprintf('Task 9 (i): Inner wall reaches %.1f°C at T = %.1f s\n', ... T_target, Twarm); break end end %% --- Plot inner wall temperature evolution figure(9) plot(timeVec(1:k), innerWallTemp(1:k), 'LineWidth', 2) hold on yline(T_target,'r--','67°C','LineWidth',1.5) xlabel('Time [s]') ylabel('Average inner wall temperature [°C]') title('Heating of the inner ceramic wall') grid on