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main.m% Define the properties of the fixed beam L = 1; % Length of beam E = 200e9; % Young's Modulus in Pa I = 4.17e-6; % Area moment of inertia in m^4 % Create finite element model num_elements = 10; elements = linspace(0, L, num_elements + 1); nodes = elements(1:end-1); % Construct global stiffness matrix K_global = zeros(num_elements + 1, num_elements + 1); for i = 1:num_elements length = elements(i + 1) - elements(i); Ke = [12, 6*length, -12, 6*length; 6*length, 4*length^2, -6*length, 2*length^2; -12, -6*length, 12, -6*length; 6*length, 2*length^2, -6*length, 4*length^2]; index = [i, i+1, i, i+1]; for j = 1:4 for k = 1:4 K_global(index(j), index(k)) = K_global(index(j), index(k)) + (E*I/length^3) * Ke(j, k); end end end % Apply boundary conditions for fixed beam (simulating fixed support) K_reduced = K_global(2:end, 2:end); % Calculate deflection (displacement) by solving for the nodal displacements F = zeros(num_elements, 1); % Assuming no external forces applied U = K_reduced\F; 1093 chars37 lines
% Define the properties of the fixed beam L = 1; % Length of beam E = 200e9; % Young's Modulus in Pa I = 4.17e-6; % Area moment of inertia in m^4 % Create finite element model num_elements = 10; elements = linspace(0, L, num_elements + 1); nodes = elements(1:end-1); % Construct global stiffness matrix K_global = zeros(num_elements + 1, num_elements + 1); for i = 1:num_elements length = elements(i + 1) - elements(i); Ke = [12, 6*length, -12, 6*length; 6*length, 4*length^2, -6*length, 2*length^2; -12, -6*length, 12, -6*length; 6*length, 2*length^2, -6*length, 4*length^2]; index = [i, i+1, i, i+1]; for j = 1:4 for k = 1:4 K_global(index(j), index(k)) = K_global(index(j), index(k)) + (E*I/length^3) * Ke(j, k); end end end % Apply boundary conditions for fixed beam (simulating fixed support) K_reduced = K_global(2:end, 2:end); % Calculate deflection (displacement) by solving for the nodal displacements F = zeros(num_elements, 1); % Assuming no external forces applied U = K_reduced\F;
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