function Cubic_Beam_on_Winkler (load_pt) % load_pt = 1 flags that point forces and/or couples will be % input via file msh_load_pt.tmp %............................................................. % Classic cubic beam on elastic foundation, % for point loads & couples, line load % Mech 400 Adv. Mech. Materials, Rice University %............................................................. if ( nargin == 0 ) ; % check for optional data flag load_pt = 0 ; % no point source data end % if from argument count % Application and element dependent controls n_g = 2 ; % number of DOF per node (deflection, slope) n_q = 0 ; % number of quadrature points required n_r = 1 ; % number of rows in B_e matrix % Read mesh nodal input data file [n_m, n_s, P, x, y, z] = get_mesh_nodes ; % Extract EBC flags from packed integer flag P [EBC_flag] = get_ebc_flags (n_g, n_m, P) ; % unpack flags EBC_count = sum( sum ( EBC_flag > 0 ) ) ; % # of EBC if ( EBC_count == 0 ) fprintf ('WARNING: No displacement boundary condition given. \n') else fprintf ('Note: expecting %g displacement BC values. \n', EBC_count) end % if % Read mesh element input data file [n_e, n_n, n_t, el_type, nodes] = get_mesh_elements ; n_d = n_g*n_m ; % system degrees of freedom (DOF) n_i = n_g*n_n ; % number of DOF per element S = zeros (n_d, n_d) ; M = zeros (n_d, n_d) ; % stiff & mass T = zeros (n_d, 1) ; % displacements % Read EBC values, if any if ( EBC_count > 0 ) ; % need EBC data [EBC_value] = get_ebc_values (n_g, n_m, EBC_flag) ; % read data end % if any EBC data expected % Read point loads & couples data, if any, and insert in C C = zeros (n_d, 1) ; % force & moments if ( load_pt > 0 ) ; % need point loads data [C] = get_and_add_point_sources (n_g, n_m, C); % add point loads end % if any point source expected C_react = C ; % save for reaction use, before BC changes % Load the element properties array load msh_properties.tmp ; % one row per element n_prop = size(msh_properties, 1) % == 1 if homogeneous fprintf ('\n(Echoing file msh_properties.tmp) \n') Line_e (1:2) = 0 ; if ( n_prop == 1 ) E = msh_properties (1, 1) ; % material modulus I = msh_properties (1, 2) ; % section inertia Line_e (1:2) = msh_properties (1, 3:4) ; % trapezoidal line load k_f = msh_properties (1, 5) ; % foundation stiffness Rho = msh_properties (1, 6) ; % beam mass per unit length % ECHO PROPERTIES fprintf ('Homogeneous Element Properties: \n' ) fprintf ('Elastity modulus (N/m^2) = %g \n', E) fprintf ('Moment of inertia (m^4) = %g \n', I) fprintf ('Line Load (N/m) = [ %g %g ] \n', ... Line_e(1), Line_e(2)) fprintf ('Foundation stiffness (N/m^2) = %g \n', k_f) fprintf ('Mass per unit length (kg/m) = %g \n', Rho) end % if if ( n_prop > n_e ) error ('ERROR: number of property sets exceeds number of elements') end % if F_k (1:n_prop) = msh_properties (1:n_prop, 5) ; % extract foundation k's if ( any ( F_k > 0 )) % BEF pressures exist BEF = 1 ; fprintf ('\nWARNING: only deflections & foundation pressures are accurate \n') else BEF = 0 ; end % if reaction flag % GENERATE ELEMENT MATRICES AND ASSYMBLE INTO SYSTEM % Assemble n_d by n_d square matrix terms from n_e by n_e for j = 1:n_e ; % loop over elements ====>> ====>> ====>> ====>> S_e = zeros (n_i, n_i) ; % clear array NtN = zeros (n_i, n_i) ; % clear array M_e = zeros (n_i, n_i) ; % clear array C_e = zeros (n_i, 1) ; % clear arrays e_nodes = nodes (j, 1:n_n) ; % connectivity % SET ELEMENT PROPERTIES & GEOMETRY L_e = x(e_nodes(2)) - x(e_nodes(1)) ; % beam length Line_e (1:2) = 0 ; if ( n_prop > 1 ) E = msh_properties (j, 1) ; % material modulus I = msh_properties (j, 2) ; % section inertia Line_e (1:2) = msh_properties (j, 3:4) ; % trapezoidal line load k_f = msh_properties (j, 5) ; % foundation stiffness Rho = msh_properties (j, 6) ; % beam mass per unit length % ECHO PROPERTIES fprintf ('\nProperties for element %g \n', j) fprintf ('Elastity modulus (N/m^2) = %g \n', E) fprintf ('Moment of inertia (m^4) = %g \n', I) fprintf ('Line Load (N/m) = [ %g %g ] \n', ... Line_e(1), Line_e(2)) fprintf ('Foundation stiffness (N/m^2) = %g \n', k_f) fprintf ('Mass per unit length (kg/m) = %g \n', Rho) end % if % ELEMENT CONDUCTION AND INTERNAL SOURCE MATRICES % Constant cubic element & foundation stiffnesses & mass matrices S_e = (E*I/L_e^3)*[ 12, 6*L_e, -12, 6*L_e ; 6*L_e, 4*L_e^2, -6*L_e, 2*L_e^2 ; -12, -6*L_e, 12, -6*L_e ; 6*L_e, 2*L_e^2, -6*L_e, 4*L_e^2 ] ; % stiffness NtN = L_e*[ 156, 22*L_e, 54, -13*L_e ; 22*L_e, 4*L_e^2, 13*L_e, -3*L_e^2 ; 54, 13*L_e, 156, -22*L_e ; -13*L_e, -3*L_e^2, -22*L_e, 4*L_e^2 ]/420; S_e = S_e + k_f * NtN ; % add foundation stiffness before assembly M_e = Rho * NtN ; % mass matrix % Map line load to node forces & moments; C_e = p_To_F * Line_e C_e = zeros (n_i, 1) ; % clear arrays if ( any (Line_e) ) ; % then form forcing vector p_To_F = L_e * [ 21, 9 ; 3*L_e, 2*L_e ; 9, 21 ; -2*L_e -3*L_e ] / 60 ; % cubic H, linear Line % 4 x 2 * 2 x 1 = 4 x 1 result C_e = p_To_F (1:n_i, 1:n_n) * Line_e' ; % force moment @ nodes end % if or set up resultant node loads for line load % SCATTER TO (ASSEMBLE INTO) SYSTEM ARRAYS % Insert completed element matrices into system matrices [rows] = get_element_index (n_g, n_n, e_nodes); % eq numbers S (rows, rows) = S (rows, rows) + S_e ; % add to system stiffness M (rows, rows) = M (rows, rows) + M_e ; % add to system mass C (rows) = C (rows) + C_e ; % add to sys force/couples end % for each j element in mesh <<==== <<==== <<==== <<==== <<==== % ALLOCATE STORAGE FOR OPTIONAL REACTION RECOVERY if ( EBC_count > 0 ) ; % reactions occur [EBC_row, EBC_col] = save_reaction_matrices (EBC_flag, S, C); save_resultant_load_vectors (n_g, C) end % if essential BC exist (almost always true) % ENFORCE ESSENTIAL BOUNDARY CONDITIONS if ( EBC_count > 0 ) ; % reactions occur [S, C] = enforce_essential_BC (EBC_flag, EBC_value, S, C); end % if essential BC exist (almost always true) % COMPUTE SOLUTION & SAVE T = S \ C ; % Compute displacements & rotations list_save_beam_displacements (n_g, n_m, T) ; % save and print % GRAPHS if ( BEF == 1 ) % plot foundation pressure cubic_beam_pressure (F_k) % graph pause (5) % display for 5 seconds end % if cubic_beam_deflection (1) % plot the beam deflection % cubic_beam_deflection (2) % plot the beam slope % OPTIONAL REACTION RECOVERY & SAVE if ( EBC_count > 0 ) ; % reactions exist ? [EBC_react] = recover_reactions_print_save (n_g, n_d, ... EBC_flag, EBC_row, EBC_col, T); % reaction to EBC end % if EBC exist % POST-PROCESS ELEMENT REACTIONS (MEMBER FORCES) fprintf ('\nIndividual Element Load and Reaction Summaries: \n') fprintf ('(F_1, M_1, F_2, M_2) \n') for j = 1:n_e ; % loop over elements ====>> ====>> ====>> ====>> ====>> e_nodes = nodes (j, 1:n_n) ; % connectivity [rows] = get_element_index (n_g, n_n, e_nodes) ; % eq numbers T_e (1:n_i) = T(rows) ; % gather element displacements % SET ELEMENT PROPERTIES & GEOMETRY L_e = x(e_nodes(2)) - x(e_nodes(1)) ; % beam length Line_e (1:2) = 0 ; if ( n_prop > 1 ) E = msh_properties (j, 1) ; % material modulus I = msh_properties (j, 2) ; % section inertia Line_e (1:2) = msh_properties (j, 3:4) ; % trapezoidal line load k_f = msh_properties (j, 5) ; % foundation stiffness end % if % ELEMENT CONDUCTION AND INTERNAL SOURCE MATRICES % Constant cubic element & foundation stiffnesses & mass matrices S_e = (E*I/L_e^3)*[ 12, 6*L_e, -12, 6*L_e ; 6*L_e, 4*L_e^2, -6*L_e, 2*L_e^2 ; -12, -6*L_e, 12, -6*L_e ; 6*L_e, 2*L_e^2, -6*L_e, 4*L_e^2 ] ; % stiffness NtN = L_e*[ 156, 22*L_e, 54, -13*L_e ; 22*L_e, 4*L_e^2, 13*L_e, -3*L_e^2 ; 54, 13*L_e, 156, -22*L_e ; -13*L_e, -3*L_e^2, -22*L_e, 4*L_e^2 ]/420; % Map line load to node forces & moments; C_e = p_To_F * Line_e C_e = zeros (n_i, 1) ; % clear arrays if ( any (Line_e) ) ; % then form forcing vector p_To_F = L_e * [ 21, 9 ; 3*L_e, 2*L_e ; 9, 21 ; -2*L_e -3*L_e ] / 60 ; % cubic H, linear Line % 4 x 2 * 2 x 1 = 4 x 1 result C_e = p_To_F (1:n_i, 1:n_n) * Line_e' ; % force moment @ nodes end % if or set up resultant node loads for line load % Assign any point force/couple to the first element with that node if ( j == 1 ) % first element only gets sources from both nodes C_e = C_e + C_react (rows) ; else C_e (3:4) = C_e (3:4) + C_react (rows(3:4)) ; % cubic beam ONLY !! end % if fprintf ('\nGiven Resultant Loading on Member %g, \n', j) disp (C_e') % Finally, get the reactions C_m = S_e * T_e' - C_e ; if ( BEF ) % add foundation resultants C_f = -k_f * NtN * T_e' ; fprintf ('Resultant Foundation Loading on Member %g, \n', j) disp (C_f') C_m = C_m - C_f ; end % if fprintf ('Net Resultant End Reactions on Member %g, \n', j) disp (C_m') end % for each j element in mesh <<==== <<==== <<==== <<==== <<==== % End finite element calculations. % See /home/mech517/public_html/Matlab_Plots for graphic options % http://www.owlnet.rice.edu/~mech517/help_plot.html for help % end of Beam_on_Winkler % +++++++++++++ functions in alphabetical order +++++++++++++++++ function cubic_beam_deflection (i_p) % Copyright 2004, J.E. Akin. All rights reserved. % ------------------------------------------------------ % Matlab graph of i_p-th component value of beam % 1=deflection, 2=slope % ------------------------------------------------------ % c_x = x coordinates of nod_per_el line polygon % c_y = y coordinates of nod_per_el line polygon % msh_typ_nodes = connectivity list for elements % loop = corners for nod_per_el line polygon % nod_per_el = Nodes per element % np = Number of Points % nt = Number of elements pre_e = 0 ; % Element items before connectivity list pre_p = 1; % Nodal items before coordinates % msh_bc_xyz = Nodal coordinates (with preceeding data) % t_x = x coordinates of nod_per_el corners % t_y = y coordinates of nod_per_el corners if ( nargin == 0 ) i_p = 1 ; end % if Pts_wide = 2 ; % fat lines % Read coordinate file and connectivity file % integer bc code, real xy pairs for np points (pre_p = 1) load msh_bc_xyz.tmp ; % Set control data: number of points np = size (msh_bc_xyz,1) ; % number of nodal points %b fprintf ('Read %g mesh coordinate pairs \n', np) ns = size (msh_bc_xyz,2) - pre_p ; % space dimension if ( ns > 1 ) fprintf ('Not 1D: will use x-coordinate only \n') end % if not 2D data % Set control data: number elements load msh_typ_nodes.tmp ; % nod_per_el nodes per element nt = size (msh_typ_nodes,1) ; % number of elements in mesh nod_per_el = size (msh_typ_nodes,2) - pre_e -1 ; % nodes per elem %b fprintf ('Read %g elements connections \n', nt) load node_results.tmp nr = size (node_results, 1); if ( nr == 0 ) error ('Error missing file node_results.tmp') end % if error max_p = size (node_results, 2) ; % number of columns H (2) = 0. ; HC1 (4) = 0. ; DHC1 (4) = 0. ; x (np) = 0. ; % pre-allocate array x t_nodes (nod_per_el) = 0 ; % Optional pre-allocation t_x (nod_per_el) = 0 ; % Optional pre-allocation t_y (nod_per_el) = 0 ; % Optional pre-allocation c_x (nod_per_el + 1) = 0 ; % Optional pre-allocation c_y (nod_per_el + 1) = 0 ; % Optional pre-allocation loop = [1:nod_per_el] ; % default to sequential order % msh_bc_xyz has: pre_p items then: x, y x = msh_bc_xyz (1:np, (pre_p+1)) ; % extract x column xmax = max (x) ; xmin = min (x) ; y = node_results(:, 1) ; dy = node_results(:, 2) ; clf % clear graphics hold on % hold image for plots xlabel (['X, Node at 45 deg (', int2str(nod_per_el), ... ' per element), Element at 90 deg']) % Loop over all elements ymax = max (node_results(:, i_p)) ; ymin = min (node_results(:, i_p)) ; el_max = ymax ; el_min = ymin ; for it = 1:nt ; % Extract element connectivity t_nodes = msh_typ_nodes (it, (pre_e+2):(nod_per_el+pre_e+1)); % Skip point elements, if any if ( all (t_nodes) ) % then valid line % Extract element coordinates & values t_x = x (t_nodes) ; % x at those nodes, only A = t_x(2) - t_x(1) ; % element length t_y = y (t_nodes) ; % y at those nodes, only t_dy = dy (t_nodes) ; % dy at those nodes, only D (1:2:4) = t_y ; D (2:2:4) = t_dy ; % Loop over local points on the cubic polynomial element n_poly = ceil ( 95 / nt) ; for k = 1: (n_poly + 1) % points in parametric space % get element parametric interpolation functions R = (k - 1)/n_poly ; % on 0 to 1 X = 2*R - 1 ; % on -1 to 1 % H = ELEMENT CUBIC SHAPE FUNCTIONS % X = LOCAL COORDINATE OF POINT, -1 TO +1 % LOCAL NODE COORD. ARE -1,+1 1------------2 H (1) = 0.5*(1 - X) ; H (2) = 0.5*(1 + X) ; x_el (k) = H * t_x ; % true X value HC1(1) = (2 - 3*X + X^3)/4; HC1(2) = (1 - X - X^2 + X^3)*A/8; HC1(3) = (2 + 3*X - X^3)/4; HC1(4) = (-1 - X + X^2 + X^3)*A/8; y_el (k) = HC1 * D' ; % true y value DHC1(1) = (-3 + 3*X*X) * 0.5 / A; DHC1(2) = (-1 - 2*X + 3*X*X) * 0.25 ; DHC1(3) = ( 3 - 3*X*X) * 0.5d0 / A; DHC1(4) = (-1 + 2*X + 3*X*X) * 0.25; dy_el (k) = DHC1 * D' ; % true dy value end % for k format short plot (x, y, 'ko') % nodal value symbols if ( i_p == 1 ) r_el = y_el ; elseif ( i_p == 2 ) r_el = dy_el ; end % if % elem max, min values [V_X, L_X] = max (r_el) ; [V_N, L_N] = min (r_el); if ( V_X > el_max ) el_max = V_X ; end if ( V_N < el_min ) el_min = V_N ; end plot (x_el, r_el, 'b-', 'LineWidth',Pts_wide) % Plot the element number x_bar = sum (t_x' )/nod_per_el ; y_bar = mean (r_el) ; t_text = sprintf (' (%g)', it); % offset # from pt text (x_bar, y_bar, t_text) % incline end % if zero in connectivity end % for all elements if ( el_max > ymax ) fprintf ('Max interior value was %g \n', el_max) ymax = el_max ; end % if if ( el_min < ymin ) ymin = el_min ; fprintf ('Min interior value was %g \n', el_min) end % if axis ([xmin, xmax, ymin, ymax]) % set axes null (1:np) = 0.5*(ymax + ymin) ; R_x = max (node_results(:, i_p)) ; R_n = min (node_results(:, i_p)) ; if ( i_p == 1 ) ylabel (['Displacement (nodal max = ', ... num2str(R_x), ', min = ', num2str(R_n), ')']) title(['Beam Displacement: ', int2str(nt),' Elements, ', ... int2str(np), ' Nodes, (', int2str(nod_per_el), ... ' per Element)']) elseif ( i_p == 2 ) ylabel (['Slope (nodal max = ', ... num2str(R_x), ', min = ', num2str(R_n), ')']) title(['Beam Slope: ', int2str(nt),' Elements, ', ... int2str(np), ' Nodes, (', int2str(nod_per_el), ... ' per Element)']) end % if % plot node points on axis inc_p = 1 ; if ( inc_p > 0 ) for i = 1:np t_text = sprintf (' %g', i); % offset # from pt text (x(i), null(i), t_text, 'Rotation', 45) % incline end % for all plot (x, null, 'k*') end % if grid print -dpng deflection_plot hold off fprintf ('Saved deflection plot as deflection_plot.png \n') % end of cubic_beam_deflection function cubic_beam_pressure (F_k) % Copyright 2008, J.E. Akin. All rights reserved. % ------------------------------------------------------ % Matlab graph of BEF pressure distribution m % ------------------------------------------------------ % c_x = x coordinates of nod_per_el line polygon % c_y = y coordinates of nod_per_el line polygon % msh_typ_nodes = connectivity list for elements % loop = corners for nod_per_el line polygon % nod_per_el = Nodes per element % np = Number of Points % nt = Number of elements pre_e = 0 ; % Element items before connectivity list pre_p = 1; % Nodal items before coordinates % msh_bc_xyz = Nodal coordinates (with preceeding data) % t_x = x coordinates of nod_per_el corners % t_y = y coordinates of nod_per_el corners i_p = 1 ; % temp n_fk = size (F_k, 2) ; % number of different foundationS % Read coordinate file and connectivity file % integer bc code, real xy pairs for np points (pre_p = 1) load msh_bc_xyz.tmp ; % Set control data: number of points np = size (msh_bc_xyz,1) ; % number of nodal points %b fprintf ('Read %g mesh coordinate pairs \n', np) ns = size (msh_bc_xyz,2) - pre_p ; % space dimension if ( ns > 1 ) fprintf ('Not 1D: will use x-coordinate only \n') end % if not 2D data null (1:np) = 0 ; Pts_wide = 2 ; % fat lines % Set control data: number elements load msh_typ_nodes.tmp ; % nod_per_el nodes per element nt = size (msh_typ_nodes,1) ; % number of elements in mesh nod_per_el = size (msh_typ_nodes,2) - pre_e -1 ; % nodes per elem %b fprintf ('Read %g elements connections \n', nt) load node_results.tmp nr = size (node_results, 1); if ( nr == 0 ) error ('Error missing file node_results.tmp') end % if error max_p = size (node_results, 2) ; % number of columns H (2) = 0. ; HC1 (4) = 0. ; DHC1 (4) = 0. ; x (np) = 0. ; % pre-allocate array x t_nodes (nod_per_el) = 0 ; % Optional pre-allocation t_x (nod_per_el) = 0 ; % Optional pre-allocation t_y (nod_per_el) = 0 ; % Optional pre-allocation c_x (nod_per_el + 1) = 0 ; % Optional pre-allocation c_y (nod_per_el + 1) = 0 ; % Optional pre-allocation loop = [1:nod_per_el] ; % msh_bc_xyz has: pre_p items then: x, y x = msh_bc_xyz (1:np, (pre_p+1)) ; % extract x column xmax = max (x) ; xmin = min (x) ; y = node_results(:, 1) ; dy = node_results(:, 2) ; clf % clear graphics hold on % hold image for plots xlabel (['X, Node at 45 deg (', int2str(nod_per_el), ... ' per element), Element at 90 deg']) % Loop over all elements Pmax = -max (node_results(:, i_p)) * max (F_k) ; Pmin = -min (node_results(:, i_p)) * max (F_k) ; el_max = Pmax ; el_min= Pmin ; % Loop over all elements for it = 1:nt ; % Element foundation stiffness, if any if ( n_fk == 1 ) % then homogeneous k_f = F_k (1) ; else k_f = F_k (it) ; end % if % Extract element connectivity t_nodes = msh_typ_nodes (it, (pre_e+2):(nod_per_el+pre_e+1)); % Skip point elements, if any if ( all (t_nodes) ) % then valid line % Extract element coordinates & values t_x = x (t_nodes) ; % x at those nodes, only A = t_x(2) - t_x(1) ; % element length t_y = y (t_nodes) ; % y at those nodes, only t_dy = dy (t_nodes) ; % dy at those nodes, only D (1:2:4) = t_y ; D (2:2:4) = t_dy ; % Loop over local points on the cubic polynomial element n_poly = ceil ( 95 / nt) ; for k = 1: (n_poly + 1) % points in parametric space % get element parametric interpolation functions R = (k - 1)/n_poly ; % on 0 to 1 X = 2*R - 1 ; % on -1 to 1 % H = ELEMENT CUBIC SHAPE FUNCTIONS % X = LOCAL COORDINATE OF POINT, -1 TO +1 % LOCAL NODE COORD. ARE -1,+1 1------------2 H (1) = 0.5*(1 - X) ; H (2) = 0.5*(1 + X) ; x_el (k) = H * t_x ; % true X value HC1(1) = (2 - 3*X + X^3)/4; HC1(2) = (1 - X - X^2 + X^3)*A/8; HC1(3) = (2 + 3*X - X^3)/4; HC1(4) = (-1 - X + X^2 + X^3)*A/8; y_el (k) = HC1 * D' ; % true y value end % for k p_el = -y_el * k_f ; % true pressure plot(x_el, p_el, 'b-', 'LineWidth',Pts_wide) % Plot the element number x_bar = mean (x_el) ; y_bar = mean (p_el) ; t_text = sprintf (' (%g)', it); % offset # from pt text (x_bar, y_bar, t_text) % incline format short max_el = max (p_el) ; min_el = min (p_el) ; if ( max_el > el_max ) el_max = max_el ; end % if if ( min_el < el_min ) el_min = min_el ; end % if end % if has non-zero nodes end % for all elements fprintf ('Max interior pressure was %g \n', el_max) fprintf ('Min interior pressure was %g \n', el_min) % plot node points on axis inc_p = 1 ; if ( inc_p > 0 ) for i = 1:np t_text = sprintf (' %g', i); % offset # from pt text (x(i), null(i), t_text, 'Rotation', 45) % incline end % for all plot (x, null, 'k*') end % if ylabel (['Pressure (nodal max = ', ... num2str(Pmax), ', min = ', num2str(Pmin), ')']) title(['Foundation Pressure: ', int2str(nt),' Elements, ', ... int2str(np), ' Nodes, (', int2str(nod_per_el), ... ' per Element)']) grid print -dpng pressure_plot hold off fprintf ('Saved pressure plot as pressure_plot.png \n') % end of cubic_beam_pressure function [S, C] = enforce_essential_BC (EBC_flag, EBC_value, S, C) % modify system linear eqs for essential boundary conditions % (by trick to avoid matrix partitions, loses reaction data) n_d = size (C, 1) ; % number of DOF eqs if ( size (EBC_flag, 2) > 1 ) ; % change to vector copy flag_EBC = reshape ( EBC_flag', 1, n_d) ; value_EBC = reshape ( EBC_value', 1, n_d) ; else flag_EBC = EBC_flag ; value_EBC = EBC_value ; end % if for j = 1:n_d % check all DOF for essential BC if ( flag_EBC (j) ) % then EBC here % Carry known columns*EBC to RHS. Zero that column and row. % Insert EBC identity, 1*EBC_dof = EBC_value. EBC = value_EBC (j) ; % recover EBC value C (:) = C (:) - EBC * S (:, j) ; % carry known column to RHS S (:, j) = 0 ; S (j, :) = 0 ; % clear, restore symmetry S (j, j) = 1 ; C (j) = EBC ; % insert identity into row end % if EBC for this DOF end % for over all j-th DOF % end enforce_essential_BC (EBC_flag, EBC_value, S, C) function [C] = get_and_add_point_sources (n_g, n_m, C) load msh_load_pt.tmp ; % node, DOF, value (eq. number) n_u = size(msh_load_pt, 1) ; % number of point sources if ( n_u < 1 ) ; % missing data error ('No load_pt data in msh_load_pt.tmp') end % if user error fprintf ('\nRead %g point sources. \n', n_u) fprintf ('(Echo of file msh_load_pt.tmp) \n') fprintf ('Node, DOF (1=force, 2=couple), Source_value \n') for j = 1:n_u ; % non-zero Neumann pts node = msh_load_pt (j, 1) ; % global node number DOF = msh_load_pt (j, 2) ; % local DOF number value = msh_load_pt (j, 3) ; % point source value fprintf ('%g %g %g \n', node, DOF, value) Eq = n_g * (node - 1) + DOF ; % row in system matrix C (Eq) = C (Eq) + value ; % add to system column matrix end % for each EBC % end get_and_add_point_sources (n_g, n_m, C) function [EBC_flag] = get_ebc_flags (n_g, n_m, P) EBC_flag = zeros(n_m, n_g) ; % initialize for k = 1:n_m ; % loop over all nodes if ( P(k) > 0 ) ; % at least one EBC here [flags] = unpack_pt_flags (n_g, k, P(k)) ; % unpacking EBC_flag (k, 1:n_g) = flags (1:n_g) ; % populate array end % if EBC at node k end % for loop over all nodes % end get_ebc_flags function [EBC_value] = get_ebc_values (n_g, n_m, EBC_flag) EBC_value = zeros(n_m, n_g) ; % initialize to zero load msh_ebc.tmp ; % node, DOF, value (eq. number) n_c = size(msh_ebc, 1) ; % number of constraints fprintf ('\nApplied Displacement Boundary Conditions: %g \n', n_c) fprintf ('(Echo of file load msh_ebc.tmp) \n') fprintf ('Node, DOF (1=displacement, 2=slope), Value. \n') disp(msh_ebc) ; % echo input for j = 1:n_c ; % loop over ebc inputs node = round (msh_ebc (j, 1)) ; % node in mesh DOF = round (msh_ebc (j, 2)) ; % DOF # at node value = msh_ebc (j, 3) ; % EBC value % Eq = n_g * (node - 1) + DOF ; % row in system matrix EBC_value (node, DOF) = value ; % insert value in array if ( EBC_flag (node, DOF) == 0 ) % check data consistency fprintf ('WARNING: EBC but no flag at node %g & DOF %g. \n', ... node, DOF) % EBC_flag (node, DOF) = 1; % try to recover from data error end % if common user error end % for each EBC EBC_count = sum (sum ( EBC_flag > 0 )) ; % check input data if ( EBC_count ~= n_c ) ; % probable user error fprintf ('\nWARNING: mismatch in bc_flag count & msh_ebc.tmp \n') end % if user error % end get_ebc_values function [rows] = get_element_index (n_g, n_n, e_nodes) % calculate system DOF numbers of element, for gather, scatter rows = zeros (1, n_g*n_n) ; % allow for node = 0 for k = 1:n_n ; % loop over element nodes global_node = round (e_nodes (k)) ; % corresponding sys node for i = 1:n_g ; % loop over DOF at node eq_global = i + n_g * (global_node - 1) ; % sys DOF, if any eq_element = i + n_g * (k - 1) ; % el DOF number if ( eq_global > 0 ) ; % check node=0 trick rows (1, eq_element) = eq_global ; % valid DOF > 0 end % if allow for omitted nodes end % for DOF i % end local DOF loop end % for each element node % end local node loop % end get_element_index function [n_e, n_n, n_t, el_type, nodes] = get_mesh_elements () ; % input file controls (for various data generators) load msh_typ_nodes.tmp ; % el_type, connectivity list (3) n_e = size (msh_typ_nodes,1) ; % number of elements if ( n_e == 0 ) ; % data file missing error ('Error missing file msh_typ_nodes.tmp') end % if error n_n = size (msh_typ_nodes,2) - 1 ; % nodes per element fprintf ('(Echo of file msh_typ_nodes.tmp) \n') fprintf ('Read %g elements with (ignored) type & %g nodes each. \n', ... n_e, n_n) el_type = round (msh_typ_nodes(:, 1)); % el type number >= 1 n_t = max(el_type) ; % number of element types %b fprintf ('Maximum number of element types = %g. \n', n_t) nodes (1:n_e, 1:n_n) = msh_typ_nodes (1:n_e, 2:1+n_n); disp(msh_typ_nodes (:, 1:1+n_n)) % echo data % end get_mesh_elements function [n_m, n_s, P, x, y, z] = get_mesh_nodes () ; % input file controls (for various data generators) % READ MESH AND EBC_FLAG INPUT DATA % specific problem data from MODEL data files (sequential) load msh_bc_xyz.tmp ; % bc_flag, x-, y-, z-coords n_m = size (msh_bc_xyz,1) ; % number of nodal points in mesh if ( n_m == 0 ) ; % data missing ! error ('Error missing file msh_bc_xyz.tmp') end % if error n_s = size (msh_bc_xyz,2) - 1 ; % number of space dimensions fprintf ('Read %g nodes. \n', n_m) fprintf ('(Echo of file msh_bc_xyz.tmp) \n') fprintf ('bc_flag, x-coordinate \n') msh_bc_xyz (:, 1)= round (msh_bc_xyz (:, 1)); P = msh_bc_xyz (1:n_m, 1) ; % integer Packed BC flag x = msh_bc_xyz (1:n_m, 2) ; % extract x column y (1:n_m, 1) = 0.0 ; z (1:n_m, 1) = 0.0 ; % default to zero if (n_s > 1 ) ; % check 2D or 3D y = msh_bc_xyz (1:n_m, 3) ; % extract y column end % if 2D or 3D if ( n_s == 3 ) ; % check 3D z = msh_bc_xyz (1:n_m, 4) ; % extract z column end % if 3D %b disp(msh_bc_xyz (:, 1:1+n_s)) ; % echo data for j = 1:n_m fprintf (' %2.2i %g \n', P(j), x(j) ) %bfprintf (' %2.2i %g %g \n', P(j), x(j), y(j) ) %bfprintf (' %2.2i %g %g %g \n', P(j), x(j), y(j), z(j) ) end % for % end get_mesh_nodes function list_save_beam_displacements (n_g, n_m, T) fprintf('\nCalculated Displacements: \n') fprintf('Node, Y_displacement, Z_rotation at %g nodes \n', n_m) T_matrix = reshape (T, n_g, n_m)' ; % pretty shape % save results (displacements) to MODEL file: node_results.tmp fid = fopen('node_results.tmp', 'w') ; % open for writing for j = 1:n_m ; % node loop, save displ fprintf (fid, '%g %g \n', T_matrix (j, 1:n_g)) ; % to file fprintf ('%g %g %g \n', j, T_matrix (j, 1:n_g)) ; % to screen end % for j DOF % end list_save_beam_displacements (n_g, n_m, T) function list_save_displacements_results (n_g, n_m, T) fprintf ('\n') ; fprintf('X_disp Y_disp Z_disp at %g nodes \n', n_m) T_matrix = reshape (T, n_g, n_m)' ; % pretty shape disp (T_matrix) ; % print displacements % save results (displacements) to MODEL file: node_results.tmp fid = fopen('node_results.tmp', 'w') ; % open for writing for j = 1:n_m ; % save displacements if ( n_g == 1 ) fprintf (fid, '%g \n', T_matrix (j, 1:n_g)) ; elseif ( n_g == 2 ) fprintf (fid, '%g %g \n', T_matrix (j, 1:n_g)) ; elseif ( n_g == 3 ) fprintf (fid, '%g %g %g \n', T_matrix (j, 1:n_g)) ; elseif ( n_g == 4 ) fprintf (fid, '%g %g %g %g \n', T_matrix (j, 1:n_g)) ; elseif ( n_g == 5 ) fprintf (fid, '%g %g %g %g %g \n', T_matrix (j, 1:n_g)) ; elseif ( n_g == 6 ) fprintf (fid, '%g %g %g %g %g %g \n', T_matrix (j, 1:n_g)) ; else error ('reformat list_save_displacements_results for n_g > 6.') end % if end % for j DOF % end list_save_displacements_results (T) function [EBC_react] = recover_reactions_print_save (n_g, n_d, ... EBC_flag, EBC_row, EBC_col, T) % get EBC reaction values by using rows of S & C (before EBC) n_d = size (T, 1) ; % number of system DOF % n_c x 1 = n_c x n_d * n_d x 1 + n_c x 1 EBC_react = EBC_row * T - EBC_col ; % matrix reactions (+-) % save reactions (forces) to MODEL file: node_reaction.tmp fprintf ('\nRecovered Reactions at Displacement or Slope BC: %g \n', ... sum (sum (EBC_flag > 0))) ; % header fprintf ('Node, DOF (1=force, 2=couple), Value \n') fid = fopen('node_reaction.tmp', 'w') ; % open for writing if ( size (EBC_flag, 2) > 1 ) ; % change to vector copy flag_EBC = reshape ( EBC_flag', 1, n_d) ; % changed else flag_EBC = EBC_flag ; % original vector end % if Totals = zeros (1, n_g) ; % zero input totals kount = 0 ; % initialize counter for j = 1:n_d ; % extract all EBC reactions if ( flag_EBC(j) ) ; % then EBC here % Output node_number, component_number, value, equation_number kount = kount + 1 ; % copy counter node = ceil(j/n_g) ; % node at DOF j j_g = j - (node - 1)*n_g ; % 1 <= j_g <= n_g React = EBC_react (kount, 1) ; % reaction value fprintf ( fid, '%g %g %g \n', node, j_g, React);% save fprintf ('%g %g %g \n', node, j_g, React); % print Totals (j_g) = Totals (j_g) + React ; % sum all components end % if EBC for this DOF end % for over all j-th DOF fprintf ('Total force and couple = ') ; disp(Totals) ; % echo total % end recover_reactions_print_save (EBC_row, EBC_col, T) function [EBC_row, EBC_col] = save_reaction_matrices (EBC_flag, S, C) n_d = size (C, 1) ; % number of system DOF EBC_count = sum (sum (EBC_flag)) ; % count EBC & reactions EBC_row = zeros(EBC_count, n_d) ; % reaction data EBC_col = zeros(EBC_count, 1) ; % reaction data if ( size (EBC_flag, 2) > 1 ) ; % change to vector copy flag_EBC = reshape ( EBC_flag', 1, n_d) ; % changed else flag_EBC = EBC_flag ; % original vector end % if kount = 0 ; % initialize counter for j = 1:n_d % System DOF loop, check for displacement BC if ( flag_EBC (j) ) ; % then EBC here % Save reaction data to be destroyed by EBC solver trick kount = kount + 1 ; % copy counter EBC_row(kount, 1:n_d) = S (j, 1:n_d) ; % copy reaction data EBC_col(kount, 1) = C (j) ; % copy reaction data end % if EBC for this DOF end % for over all j-th DOF % end sys DOF loop % end save_reaction_matrices (S, C, EBC_flag) function save_resultant_load_vectors (n_g, C) % save resultant forces to MODEL file: node_resultants.tmp n_d = size (C, 1) ; % number of system DOF fprintf ('\nResultants of all input sources: \n') fprintf ('Node, DOF (1=force, 2=couple), Value \n') fid = fopen('node_resultant.tmp', 'w'); % open for writing Totals = zeros (1, n_g) ; % zero input totals for j = 1:n_d ; % extract all resultants if ( C (j) ~= 0. ) ; % then source here % Output node_number, component_number, value, equation_number node = ceil(j/n_g) ; % node at DOF j j_g = j - (node - 1)*n_g ; % 1 <= j_g <= n_g value = C (j) ; % resultant value fprintf ( fid, '%g %g %g %g \n', node, j_g, value, j);% save fprintf ('%g %g %g \n', node, j_g, value); % print Totals (j_g) = Totals (j_g) + value ; % sum all inputs end % if non-zero for this DOF end % for over all j-th DOF fprintf ('Totals = ') ; disp(Totals) ; % echo totals % end save_resultant_load_vectors (n_g, n_m, C) function [flags] = unpack_pt_flags (n_g, N, flag) % unpack n_g integer flags from the n_g digit flag at node N % integer flag contains (left to right) f_1 f_2 ... f_n_g full = flag ; % copy integer check = 0 ; % validate input for Left2Right = 1:n_g ; % loop over local DOF at k Right2Left = n_g + 1 - Left2Right ; % reverse direction work = floor (full / 10) ; % work item keep = full - work * 10 ; % work item flags (Right2Left) = keep ; % insert into array full = work ; % work item check = check + keep * 10^(Left2Right - 1) ; % validate end % for each local DOF if ( flag > check ) ; % check for likely error fprintf ('WARNING: bc flag likely reversed at node %g. \n', N) end % if likely user error % end unpack_pt_flags %=================== Running gives ===================================== % >> Cubic_Beam_on_Foundation(1) % Read 5 nodes with bc_flag & 1 coordinates. % (Echo of file msh_bc_xyz.tmp) % 10 -60 % 0 -30 % 0 -8 % 10 40 % 0 60 % % Note: expecting 2 displacement BC values. % % Read 4 elements with (ignored) type & 2 nodes each. % (Echo of file msh_typ_nodes.tmp) % 1 1 2 % 1 2 3 % 1 3 4 % 1 4 5 % % Applied Displacement Boundary Conditions: 2 % (Echo of file load msh_ebc.tmp) % Node, DOF (1=displacement, 2=slope), Value. % 1 1 0 % 4 1 0 % % Read 1 point sources. % (Echo of file msh_load_pt.tmp) % Node, DOF (1=force, 2=couple), Source_value % 2 1 -5000 % % (Echoing file msh_properties.tmp) % Properties for element 1 % Elastity modulus (N/m^2) = 1.5e+06 % Moment of inertia (m^4) = 426.7 % Line Load (N/m) = [ 0 0 ] % Foundation stiffness (N/m^2) = 0 % Mass per unit length (kg/m) = 0 % % Properties for element 2 % Elastity modulus (N/m^2) = 1.5e+06 % Moment of inertia (m^4) = 426.7 % Line Load (N/m) = [ 0 0 ] % Foundation stiffness (N/m^2) = 0 % Mass per unit length (kg/m) = 0 % % Properties for element 3 % Elastity modulus (N/m^2) = 1.5e+06 % Moment of inertia (m^4) = 426.7 % Line Load (N/m) = [ -100 -100 ] % Foundation stiffness (N/m^2) = 0 % Mass per unit length (kg/m) = 0 % % Properties for element 4 % Elastity modulus (N/m^2) = 1.5e+06 % Moment of inertia (m^4) = 426.7 % Line Load (N/m) = [ 0 0 ] % Foundation stiffness (N/m^2) = 0 % Mass per unit length (kg/m) = 0 % % Resultants of all input sources: % Node, DOF (1=force, 2=couple), Value % 2 1 -5000 % 3 1 -2400 % 3 2 -19200 % 4 1 -2400 % 4 2 19200 % Totals = -9800 0 % % Calculated Displacements: % Node, Y_displacement, Z_rotation at 5 nodes % 1 0 -0.00730227 % 2 -0.186361 -0.00403159 % 3 -0.223254 0.000633838 % 4 0 0.00701974 % 5 0.140395 0.00701974 % Saved deflection plot as deflection_plot.png % % Recovered Reactions at Displacement or Slope BC: 2 % Node, DOF (1=force, 2=couple), Value % 1 1 4652 % 4 1 5148 % Total force and couple = 1.0e+03 * % 9.8000 0 % % Individual Element Load and Reaction Summaries: % (F_1, M_1, F_2, M_2) % Given Resultant Loading on Member 1, % 0 0 -5000 0 % Net Resultant End Reactions on Member 1, % 1.0e+05 *[ 0.0465 0 0.0035 1.3956] % % Given Resultant Loading on Member 2, % 0 0 0 0 % Net Resultant End Reactions on Member 2, % 1.0e+05 *[ -0.0035 -1.3956 0.0035 1.3190] % % Given Resultant Loading on Member 3, % -2400 -19200 -2400 19200 % Net Resultant End Reactions on Member 3, % 1.0e+05 *[ -0.0035 -1.3190 0.0515 -0.0000] % % Given Resultant Loading on Member 4, % 0 0 0 0 % Net Resultant End Reactions on Member 4, % 0 0 0 0 % >> quit