function Modular_Plane_Stress_XY (load_pt, pre_p, pre_e)
%.............................................................
%     Plane Stress with body and point loads, T3 triangle
%             XY COORDINATES CLOSED FORM INTEGRALS
%                Change E_e to get Plane Strain
%.............................................................
% pre_e = # of dummy items before el_type & connectivity
% pre_p = # of dummy items before BC_flag % coordinates
if ( nargin == 2 )                ;  % check for optional data
  pre_e = 0                       ;  % no el # in msh_typ_nodes  
elseif ( nargin == 1 )            ;  % check for optional data
  pre_p = 0 ; pre_e = 0           ;  % no pt # in msh_bc_xyz     
elseif ( nargin == 0 )            ;  % check for optional data
  load_pt = 0 ; pre_p = 0 ; pre_e = 0 ; % no point source data
end % if from argument count

%         Application and element dependent controls
n_g = 2                  ; % number of DOF per node (temperature)
n_q = 1                  ; % number of quadrature points required
n_r = 3                  ; % number of rows in B_e matrix

%              Read mesh input data files
[n_m, n_s, P, x, y, z]          = get_mesh_nodes    (pre_p) ;
[n_e, n_n, n_t, el_type, nodes] = get_mesh_elements (pre_e) ;
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) ; C = zeros (n_d, 1)      ; % initalize sums

%      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
fprintf ('Note: expecting %g EBC values. \n', EBC_count)
 
%                  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 Neumann point loads data, if any, and insert in C
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

%  ============== ASSUMING HOMOGENOUS PROPERTIES =================

%    GENERATE ELEMENT MATRICES AND ASSYMBLE INTO SYSTEM
%  Assemble n_d by n_d square matrix terms from n_e by n_e

B_e = zeros (n_r, n_i)                            ; % clear array
for j = 1:n_e                        ; % loop over elements ====>>
  S_e = zeros (n_i, n_i)                          ; % clear array
  C_b = zeros (n_i, 1) ; C_e = zeros (n_i, 1)     ; % clear arrays
  e_nodes = nodes (j, 1:n_n)                      ; % connectivity
  
%               SET ELEMENT PROPERTIES & GEOMETRY
  [t_e, Body_e, E_e] = set_constant_plane_stress_prop; % properties
  thick = t_e * el_type (j)                   ; % integer multiple 
  [a, b, c, center, two_A] = form_T3_geom_constants (x, y, e_nodes);

%      ELEMENT CONDUCTION AND INTERNAL SOURCE MATRICES 
  % for q = 1:n_q        ; % Loop over element quadrature points ---->

%   H_i (x,y) = (a_i + b_i*x + c_i*y)/two_A  % interpolations

%  define 3 by 6 strain-displacement matrix, B_e
    B_e (1, 1:2:5) = b (1:3)/two_A ; B_e (2, 2:2:6) = c (1:3)/two_A ;
    B_e (3, 1:2:5) = c (1:3)/two_A ; B_e (3, 2:2:6) = b (1:3)/two_A ;

%        stiffness matrix, with constant jacobian 
    S_e = ( B_e' * E_e * B_e ) * thick * two_A / 2; % stiffness 

%        internal body force per unit volume, Body_e
    if ( any (Body_e) )                  ; % then form forcing vector
      Hi_Bx = Body_e (1) * thick * two_A / 6.0 ; % integral H_i Body x
      Hi_By = Body_e (2) * thick * two_A / 6.0 ; % integral H_i Body y
      C_b (1:2:5) = [ Hi_Bx, Hi_Bx, Hi_Bx ]    ; % vector result 
      C_b (2:2:6) = [ Hi_By, Hi_By, Hi_By ]    ; % vector result 
      C_e = C_e + C_b                          ; % scatter   
    end % if or set up properties for body force
  % end % for loop over n_q element quadrature points          <----

%         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 sq
  C (rows) = C (rows) + C_e              ; % add to sys column
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);
end % if essential BC exist (almost always true)

%                   ECHO PROPERTIES
fprintf ('Application properties are: \n')
fprintf ('Thickness = %g \n', thick)
fprintf ('Body Force = '), disp (Body_e)
fprintf ('Elastity matrix:'), disp(E_e)

%         ENFORCE ESSENTIAL BOUNDARY CONDITIONS
save_resultant_load_vectors (n_g, C)
[S, C] = enforce_essential_BC (EBC_flag, EBC_value, S, C);

%             COMPUTE SOLUTION & SAVE
T = S \ C                                ; % Compute displacements
list_save_displacements_results (n_g, n_m, T)   ; % save and print

%          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 HEAT FLUX RECOVERY & SAVE
output_PlaneStress_stresses (n_e, n_g, n_n, n_q, nodes, x, y, T)

% 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 Modular_Plane_Stress_XY            

%  +++++++++++++ functions in alphabetical order +++++++++++++++++

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 [a, b, c, center, two_A] = form_T3_geom_constants (x, y, e_nodes)
% Planar 3 node triangle geometry: H_i (x,y) = (a_i + b_i*x + c_i*y)/two_a
%                   define nodal coordinates, ccw: i, j, k
  x_e = x(e_nodes) ; y_e = y(e_nodes)        ; % coord at el nodes
  x_i = x_e(1) ; x_j = x_e(2) ; x_k = x_e(3) ; % change notation
  y_i = y_e(1) ; y_j = y_e(2) ; y_k = y_e(3) ; % change notation

%  define centroid coordinates (quadrature point)
  center (1) = (x_i + x_j + x_k)/3 ;  
  center (2) = (y_i + y_j + y_k)/3 ;

%  geometric parameters: H_i (x,y) = (a_i + b_i*x + c_i*y)/two_a
  a_i = x_j * y_k - x_k * y_j ; b_i = y_j - y_k ; c_i = x_k - x_j ;
  a_j = x_k * y_i - x_i * y_k ; b_j = y_k - y_i ; c_j = x_i - x_k ;
  a_k = x_i * y_j - x_j * y_i ; b_k = y_i - y_j ; c_k = x_j - x_i ;

  a (1:3) = [a_i, a_j, a_k] ;
  b (1:3) = [b_i, b_j, b_k] ;
  c (1:3) = [c_i, c_j, c_k] ;

%  calculate twice element area
  two_A = a_i + a_j + a_k            ; % = b_j*c_k - b_k*c_j also
% end form_T3_geom_constants (x, y, e_nodes)

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 ('Read %g point sources. \n', n_u)
  fprintf ('Node DOF 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
  fprintf ('\n')
% 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 ('Read %g EBC data with Node, DOF, Value. \n', n_c)
  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)
      %b 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 ('WARNING: mismatch in bc_flag count & msh_ebc.tmp')
  end % if user error
% end get_ebc_values

function [rows] = get_element_index (n_g, n_n, e_nodes)
rows = zeros (1, n_g*n_n) ;
for k = 1:n_n ;
  global_node = round (e_nodes (k)) ;
  for i = 1:n_g ;
    eq_global  = i + n_g * (global_node - 1) ;
    eq_element = i + n_g * (k           - 1) ;
    if ( eq_global > 0 )  
      rows (1, eq_element) = eq_global  ;
    end % if allow for omitted nodes
  end % for DOF i
end % for each element node
% end get_element_index 

function [n_e, n_n, n_t, el_type, nodes] = get_mesh_elements (pre_e) ;
% MODEL input file controls (for various data generators) 
if (nargin == 0)  ; % default to no proceeding items in data
  pre_e = 0       ; % Dummy items before el_type & connectivity 
end % if 

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) - pre_e - 1 ; % nodes per element       
fprintf ('Read %g elements with type number & %g nodes each. \n', ...
          n_e, n_n) 
el_type = round (msh_typ_nodes(:, pre_e+1)); % el type number >= 1 
n_t     = max(el_type)                   ; % number of element types 
fprintf ('Maximum number of element types = %g. \n', n_t) 
nodes (1:n_e, 1:n_n) = msh_typ_nodes (1:n_e, (pre_e+2:pre_e+1+n_n)); 
disp(msh_typ_nodes (:, (pre_e+1:pre_e+1+n_n))) % echo data
% end get_mesh_elements 

function [n_m, n_s, P, x, y, z] = get_mesh_nodes (pre_p) ;
% MODEL input file controls (for various data generators) 
if (nargin == 0) % override default 
  pre_p = 0 ; % Dummy items before BC_flag % coordinates 
end % if 
 
%       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) - pre_p - 1 ; % number of space dimensions 
fprintf ('Read %g nodes with bc_flag & %g coordinates. \n', n_m, n_s) 
msh_bc_xyz (:, (pre_p+1))= round (msh_bc_xyz (:, (pre_p+1)));
P = msh_bc_xyz (1:n_m, (pre_p+1)) ; % integer Packed BC flag 
x = msh_bc_xyz (1:n_m, (pre_p+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, (pre_p+3))           ; % extract y column  
end % if 2D or 3D
if ( n_s == 3 )                               ; % check 3D
  z = msh_bc_xyz (1:n_m, (pre_p+4))           ; % extract z column 
end % if 3D 
disp(msh_bc_xyz (:, (pre_p+1):(pre_p+1+n_s))) ; % echo data
% end get_mesh_nodes 

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 list_save_temperature_results (T)
  n_m = size (T, 1)                          ; % get size
  fprintf('Temperature at %g nodes \n', n_m) ; % header

  % save results (temperature) to MODEL file: node_results.tmp
  fid = fopen('node_results.tmp', 'w')       ; % open for writing
  for j = 1:n_m                              ; % save temperature  
    fprintf ( fid, '%g \n', T (j))           ; % print
    fprintf (' %g %g \n', j, T (j))          ; % sequential save
  end % for j DOF
% end list_save_temperature_results (T)

function output_PlaneStress_stresses(n_e, n_g, n_n, n_q, nodes, x,y,T)
%       POST-PROCESS ELEMENT STRESS RECOVERY & SAVE
fid = fopen('el_qp_xyz_fluxes.tmp', 'w')    ; % open for writing
fprintf ('\n')                              ; % blank line
fprintf('Elem, QP, X_qp, Y_qp \n')                         ;% header
fprintf('Elem, QP, Stress_qp: xx        yy          xy \n');% header
  
for j = 1:n_e                      ; % loop over elements   ====>>
  e_nodes = nodes (j, 1:n_n)               ; % connectivity
  [a, b, c, center, two_A] = form_T3_geom_constants (x, y, e_nodes);
  [t_e, Body_e, E_e] = set_constant_plane_stress_prop; % properties

%  get DOF numbers for this element, gather solution
  [rows] = get_element_index (n_g, n_n, e_nodes) ; % eq numbers
  T_e = T (rows)                          ; % gather element DOF

  for q = 1:n_q        ; % Loop over element quadrature points ---->

%   H_i (x,y) = (a_i + b_i*x + c_i*y)/two_A    % interpolations
    B_e (1, 1:2:5) = b (1:3)/two_A ; B_e (2, 2:2:6) = c (1:3)/two_A ;
    B_e (3, 1:2:5) = c (1:3)/two_A ; B_e (3, 2:2:6) = b (1:3)/two_A ;

%  COMPUTE GRADIENT & HEAT FLUX, SAVE LOCATION AND VALUES
    Strains = B_e * T_e                      ; % mechanical strain
    Stress = E_e * Strains                   ; % mechanical stress
    fprintf (fid,'%g %g %g %g %g  \n',  center(1), center(2), ...
             Stress(1), Stress(2), Stress(3));% save
    fprintf ('%g %g %g %g  \n',    j, q, center(1:2));% prt
    fprintf ('%g %g %g %g %g  \n', j, q, Stress(1:3));% prt
    fprintf ('\n')                                   ;% prt
  end % for loop over n_q element quadrature points          <----
end % for each j element in mesh  
% end output_PlaneStress_stresses (n_e, n_g, n_n, n_q, nodes, x, y, T) 

function output_T3_heat_flux (n_e, n_g, n_n, n_q, nodes, x, y, T) 
%       POST-PROCESS ELEMENT HEAT FLUX RECOVERY & SAVE
fid = fopen('el_qp_xyz_fluxes.tmp', 'w')    ; % open for writing
fprintf ('\n')                              ; % blank line
fprintf('Elem, X_qp, Y_qp, HeatFlux_x, HeatFlux_y \n');% header

for j = 1:n_e                      ; % loop over elements   ====>>
  e_nodes = nodes (j, 1:n_n)               ; % connectivity
  [a, b, c, center, two_A] = form_T3_geom_constants (x, y, e_nodes);
  [t_e, Body_e, E_e] = set_constant_plane_stress_prop; % properties

%  get DOF numbers for this element, gather solution
  [rows] = get_element_index (n_g, n_n, e_nodes) ; % eq numbers
  T_e = T (rows)                          ; % gather element DOF
  
  for q = 1:n_q        ; % Loop over element quadrature points ---->

%   H_i (x,y) = (a_i + b_i*x + c_i*y)/two_A    % interpolations
    B_e (1, 1:3) = b(1:3) / two_A            ; % dH/dx
    B_e (2, 1:3) = c(1:3) / two_A            ; % dH/dy

%  COMPUTE GRADIENT & HEAT FLUX, SAVE LOCATION AND VALUES
    Gradient = B_e * T_e                        ; % gradient vector
    HeatFlux = E_e * Gradient                   ; % heat flux vector
    fprintf (fid, '%g %g %g %g \n',  center(1:2), HeatFlux(1:2));% save
    fprintf ('%g %g %g %g %g \n', j, center(1:2), HeatFlux(1:2));% prt
  end % for loop over n_q element quadrature points          <----
end % for each j element in mesh                            <<====
% end output_T3_heat_flux (n_e, n_g, n_n, n_q, nodes, x, y, 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 ('\n')                        ; % Skip a line
  fprintf ('Node, DOF, Value, Equation Number for %g Reactions \n', ...
            sum (sum (EBC_flag > 0)))   ; % header
  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
  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 %g \n', node, j_g, React, j);% save
      fprintf ('%g %g %g %g \n', node, j_g, React, j);     % print
    end % if EBC for this DOF
  end % for over all j-th DOF
% 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
%b disp(EBC_flag)
%b disp(flag_EBC)
  kount = 0                                ; % initialize counter
  for j = 1:n_d                % check all DOF for displacement BC
    if ( flag_EBC (j) )                    ; % then EBC here
%b j
  %   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 save_reaction_matrices (S, C, EBC_flag)

function save_resultant_load_vectors (n_g, C)
  n_d = size (C, 1)                     ; % number of system DOF
  % save resultant forces to MODEL file: node_resultants.tmp
  fprintf ('\n')                        ; % Skip a line
  fprintf ('Node, DOF, Resultant Value, Equation Number \n')
  fid = fopen('node_resultant.tmp', 'w') ; % open for writing
  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 %g \n', node, j_g, value, j);     % print
    end % if non-zero for this DOF
  end % for over all j-th DOF
% end save_resultant_load_vectors (n_g, n_m, C)

function [t_e, Body_e, E_e] = set_constant_plane_stress_prop ;
  t_e = 1 ; Body_e (1:2) = 0.             ; % defaults
%                         case 1
  t_e          = 5e-3                     ; % thickness
  Body_e (1:2) = [5e5, 0.]                ; % components
  E   = 15e9                              ; % Elastic modulus
  nu  = 0.25                              ; % Poisson's ratio
%                    plane stress 
  E_v = E/(1 - nu^2)                            ; % constant
  E_e (1, 1) = E_v      ; E_e (1, 2) = E_v * nu ; % non-zero term
  E_e (2, 1) = E_v * nu ; E_e (2, 2) = E_v      ; % non-zero term
  E_e (3, 3) = E_v * (1 - nu) / 2               ; % non-zero term
%end set_constant_plane_stress_prop 

function [t_e, Q_e, E_e] = set_constant_2D_conduction_prop
 % Manually set constant element properties (Fig 11.9 text)
  Q_e = 0. ; t_e = 1.                     ; % defaults 
% case 1
  Kx  = 8. ; Ky = 8. ; Kxy = 0.           ; % thermal conductivity
% case 2
  kx  = 1. ; Ky = 1. ; Kxy = 0. ;
% insert
  E_e = zeros (2, 2)                      ; % constitutive matrix
  E_e (1, 1) = Kx   ; E_e (1, 2) = Kxy    ; % non-zero term
  E_e (2, 1) = Kxy  ; E_e (2, 2) = Ky     ; % non-zero term
% end set_constant_2D_conduction_prop

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 ===========================================
% >> Modular_Plane_Sress_XY
% Read 5 nodes with bc_flag & 2 coordinates. 
%     10     0     0
%     11     0     2
%      0     1     1
%      0     2     0
%      0     2     2
%  
%  Read 4 elements with type number & 3 nodes each. 
%  Maximum number of element types = 1. 
%       1     1     3     2
%       1     1     4     3
%       1     4     5     3
%       1     3     5     2
%  
%  Note: expecting 3 EBC values. 
%  Read 3 EBC data with Node, DOF, Value. 
%       1     1     0
%       2     1     0
%       2     2     0
%  
%  Application properties are: 
%  Thickness = 0.005 
%  Body Force =       500000           0
%  Elastity matrix:   1.0e+10 *
%      1.6000    0.4000         0
%      0.4000    1.6000         0
%           0         0    0.6000
%  
%  Node, DOF, Resultant Value, Equation Number 
%  1 1 1666.67 1 
%  2 1 1666.67 3 
%  3 1 3333.33 5 
%  4 1 1666.67 7 
%  5 1 1666.67 9 
%  
%  X_disp      Y_disp      Z_disp   at 5 nodes 
%     1.0e-04 *
%           0    0.3403
%           0         0
%      0.5243    0.1701
%      0.6667    0.1667
%      0.6667    0.1736
%  
%  Node, DOF, Value, Equation Number for 3 Reactions 
%  1 1 -5000 1 
%  1 2 5.68434e-14 2 
%  4 1 6.82121e-13 7 
%  
%  Elem, QP, X_qp, Y_qp 
%  Elem, QP, Stress_qp: xx        yy          xy 
%  1 1 0.333333 1  
%  1 1 770833 -62500 1.01644e-10  
%  
%  2 1 1 0.333333  
%  2 1 500000 -5.82077e-11 62500  
%  
%  3 1 1.66667 1  
%  3 1 229167 62500 -2.03288e-11  
%  
%  4 1 1 1.66667  
%  4 1 500000 -2.91038e-11 -62500
%  ========================== end =================================
