FEATool Multiphysics  v1.17.0
Finite Element Analysis Toolbox
ex_heat_exchanger1.m File Reference

Description

EX_HEAT_EXCHANGER1 Example of free and forced convection around a heated cylinder.

[ FEA, OUT ] = EX_HEAT_EXCHANGER1( VARARGIN ) Sets up and solves an example of temperature transport in a fluid around a heated cylinder. The model involves both free and forced convection by using the Boussinesq approximation.

Accepts the following property/value pairs.

Input       Value/{Default}        Description
-----------------------------------------------------------------------------------
hmax        scalar {0.0005}        Max grid cell size
sf_u        string {sflag2}        Shape function for velocity
sf_p        string {sflag1}        Shape function for pressure
sf_T        string {sflag1}        Shape function for temperature
solver      string {}              Solver selection default, openfoam, fenics
iplot       scalar 0/{1}           Plot solution and error (=1)
                                                                                  .
Output      Value/(Size)           Description
-----------------------------------------------------------------------------------
fea         struct                 Problem definition struct
out         struct                 Output struct

Code listing

 cOptDef = { 'hmax',     0.0004;
             'sf_u',     'sflag1';
             'sf_p',     'sflag1';
             'sf_T',     'sflag1';
             'solver',   '';
             'iplot',    1;
             'w',        0.0075;
             'h',        0.05;
             'yc',       0.02;
             'r',        0.003;
             'rho',      2.2e1;
             'miu',      2.8e-3;
             'cp',       3.1e3;
             'k',        0.55;
             'al',       0.26e-3;
             'g',        9.81;
             'vin',      40e-2;
             'Tc',       300;
             'Th',       330;
             'tol',      0.1;
             'fid',      1 };
 [got,opt] = parseopt( cOptDef, varargin{:} );
 fid       = opt.fid;


% Geometry definition.
 fea.sdim         = { 'x' 'y' };
 fea.geom.objects = { gobj_rectangle( 0, opt.w, 0, opt.h, 'R1' ) ...
                      gobj_circle( [0 opt.yc], opt.r, 'C1' ) };
 fea = geom_apply_formula( fea, 'R1-C1' );


% Grid generation.
 fea.grid = gridgen( fea, 'hmax', opt.hmax, 'fid', fid );


% Boundary conditions.
 dtol = 1e-6;
 ib_l = findbdr( fea, ['x<',num2str(dtol)] );         % Right boundary numbers.
 ib_r = findbdr( fea, ['x>',num2str(opt.w-dtol)] );   % Left boundary number.
 ib_b = findbdr( fea, ['y<',num2str(dtol)] );         % Bottom boundary number.
 ib_t = findbdr( fea, ['y>',num2str(opt.h-dtol)] );   % Top boundary number.
 ib_c = findbdr( fea, ['sqrt(x.^2+(y-',num2str(opt.yc),').^2)<',num2str(opt.r+dtol)] );   % Cylinder boundary numbers.


% Problem definition.
 fea.expr = { 'rho'   opt.rho ;
              'miu'   opt.miu ;
              'cp'    opt.cp  ;
              'k'     opt.k   ;
              'alpha' opt.al  ;
              'g'     opt.g   ;
              'vin'   opt.vin ;
              'Tc'    opt.Tc  ;
              'Th'    opt.Th  };

 fea = addphys(fea,@navierstokes);     % Add Navier-Stokes equations physics mode.
 fea.phys.ns.eqn.coef{1,end} = { 'rho' };
 fea.phys.ns.eqn.coef{2,end} = { 'miu' };
 fea.phys.ns.eqn.coef{4,end} = { 'alpha*g*rho*(T-Tc)' };
 fea.phys.ns.bdr.sel(ib_t)   = 4;      % Set pressure to zero on top boundary segment.
 fea.phys.ns.bdr.sel(ib_b)   = 2;      % Set y-velocity to vin at bottom boundary.
 fea.phys.ns.bdr.coef{2,end}{2,ib_b} = 'vin';
 fea.phys.ns.sfun            = { opt.sf_u opt.sf_u opt.sf_p };

 fea = addphys(fea,@heattransfer);     % Add heat transfer physics mode.
 fea.phys.ht.sfun            = { opt.sf_T };
 fea.phys.ht.eqn.coef{1,end} = { 'rho' };
 fea.phys.ht.eqn.coef{2,end} = { 'cp' };
 fea.phys.ht.eqn.coef{3,end} = { 'k' };
 fea.phys.ht.eqn.coef{4,end} = { fea.phys.ns.dvar{1} };
 fea.phys.ht.eqn.coef{5,end} = { fea.phys.ns.dvar{2} };
 fea.phys.ht.bdr.sel         = 3*ones( 1, max(fea.grid.b(3,:)) );   % Default to symmetry BCs.
 fea.phys.ht.bdr.sel(ib_t)   = 2;   % Set top boundary to convective flux/outflow.
 fea.phys.ht.bdr.sel([ib_c ib_b])    = 1;   % Set temperature to bottom and cylinder boundaries.
 [fea.phys.ht.bdr.coef{1,end}{ib_b}] = deal('Tc');
 [fea.phys.ht.bdr.coef{1,end}{ib_c}] = deal('Th');


% Parse and solve problem.
 fea = parsephys(fea);
 [fea.bdr.d{1}{[ib_l ib_r]}] = deal(0);    % Manually apply slip boundary conditions.
 [fea.bdr.d{2}{[ib_l ib_r]}] = deal([]);
 [fea.bdr.n{2}{[ib_l ib_r]}] = deal(0);
 fea = parseprob(fea);

 if( strcmp(opt.solver,'openfoam') )
   logfid = fid; if( ~got.fid ), fid = []; end
   fea.sol.u = openfoam( fea, 'fid', fid, 'logfid', logfid, 'nproc', 1 );
   fid = logfid;
 elseif( strcmp(opt.solver,'fenics') )
   fea = fenics( fea, 'fid', fid );
 else
   fea.sol.u = solvestat( fea, 'fid', fid, 'maxnit', 50 );
 end


% Postprocessing.
 if( opt.iplot>0 )
   figure
   subplot(1,2,1)
   postplot( fea, 'surfexpr', 'sqrt(u^2+v^2)', 'arrowexpr', {'u' 'v'} )
   hold on
   fea.grid.p(1,:) = -fea.grid.p(1,:);   % Mirror solution.
   postplot( fea, 'surfexpr', 'sqrt(u^2+v^2)', 'arrowexpr', {'u' 'v'} )
   title('Velocity field')

   subplot(1,2,2)
   postplot( fea, 'surfexpr', 'T' )
   hold on
   fea.grid.p(1,:) = -fea.grid.p(1,:);   % Mirror solution.
   postplot( fea, 'surfexpr', 'T' )
   title('Temperature')
 end

% Average temperature at outlet.
 out.T_av_out = intbdr( 'T*v', fea, ib_t )/intbdr( 'v', fea, ib_t );
 out.err = abs(intbdr('T-Tc',fea,3)/0.0075-1.7)/1.7;
 out.pass = out.err < opt.tol;


 if( nargout==0 )
   clear fea out
 end