|
FEATool Multiphysics
v1.17.5
Finite Element Analysis Toolbox
|
|
|
FEATool Multiphysics
v1.17.5
Finite Element Analysis Toolbox
|
EX_COMPRESSIBLEEULER3 2D Steady reflected shock problem.
[ FEA, OUT ] = EX_COMPRESSIBLEEULER3( VARARGIN ) Sets up and solves a steady reflected compressible Euler shock problem and compares with the analytical solution.
[1] H. W. Liepmann, A. Roshko, Elements of Gas Dynamics, Courier Corporation, 2013.
Accepts the following property/value pairs.
Input Value/{Default} Description
-----------------------------------------------------------------------------------
lev scalar {2} Grid refinement level
sfun string {sflag1} Shape function
solver string openfoam/su2/{} Use OpenFOAM, SU2, or default solver
iplot scalar 0/{1} Plot solution and error (=1)
.
Output Value/(Size) Description
-----------------------------------------------------------------------------------
fea struct Problem definition struct
out struct Output struct
cOptDef = { 'lev', 2;
'sfun', 'sflag1';
'solver', '';
'iplot', 1;
'tol', 0.15;
'fid', 1 };
[got,opt] = parseopt(cOptDef,varargin{:});
fid = opt.fid;
fea.sdim = { 'x', 'y' };
fea.geom.objects = { gobj_rectangle(0,4.1,0,1) };
lev = ceil(opt.lev);
fea.grid = rectgrid(lev*41,lev*10,[0,4.1;0,1]);
fea.grid = quad2tri(fea.grid,1);
ML = 2.9;
rL = 1;
uL = 2.9;
vL = 0;
pL = 0.714286;
th1 = 29*pi/180;
MT = 2.3781;
rT = 1.7;
uT = 2.619334;
vT = -0.5063;
pT = 1.52819;
th2 = 23*pi/180;
MR = 1.94253;
rR = 2.6872838;
uR = 2.401499;
vR = 0;
pR = 2.93398;
s = '%g-((1-y)>x*%g)*(%g-%g)*(x<%g)-(x>=%g)*(y<(x-%g)*%g)*(%g-%g)';
rref = sprintf( s, rT, atan(th1), rT, rL, 1/atan(th1), 1/atan(th1), 1/atan(th1), atan(th2), rT, rR );
uref = sprintf( s, uT, atan(th1), uT, uL, 1/atan(th1), 1/atan(th1), 1/atan(th1), atan(th2), uT, uR );
vref = sprintf( s, vT, atan(th1), vT, vL, 1/atan(th1), 1/atan(th1), 1/atan(th1), atan(th2), vT, vR );
pref = sprintf( s, pT, atan(th1), pT, pL, 1/atan(th1), 1/atan(th1), 1/atan(th1), atan(th2), pT, pR );
fea = addphys(fea,@compressibleeuler);
fea.phys.ee.prop.artstab.id_coef = 2*fea.phys.ee.prop.artstab.id_coef;
fea.phys.ee.prop.artstab.sd_coef = 2*fea.phys.ee.prop.artstab.sd_coef;
init0 = { rL, uL, vL, pL };
fea.phys.ee.eqn.coef{5,end}{1} = rL;
fea.phys.ee.eqn.coef{6,end}{1} = uL;
fea.phys.ee.eqn.coef{7,end}{1} = vL;
fea.phys.ee.eqn.coef{8,end}{1} = pL;
fea.phys.ee.bdr.sel(2) = 2;
fea.phys.ee.bdr.sel(3:4) = 1;
fea.phys.ee.bdr.coef{1,end}{1,3} = rT;
fea.phys.ee.bdr.coef{1,end}{2,3} = uT;
fea.phys.ee.bdr.coef{1,end}{3,3} = vT;
fea.phys.ee.bdr.coef{1,end}{4,3} = pT;
fea.phys.ee.bdr.coef{1,end}{1,4} = rL;
fea.phys.ee.bdr.coef{1,end}{2,4} = uL;
fea.phys.ee.bdr.coef{1,end}{3,4} = vL;
fea.phys.ee.bdr.coef{1,end}{4,4} = pL;
fea = parsephys(fea);
fea = parseprob(fea);
if( strcmp(opt.solver,'openfoam') )
logfid = fid; if( ~got.fid ), fid = []; end
fea.sol.u = openfoam( fea, 'deltaT', 0.01, 'endTime', 4, 'maxCo', 0.2, 'nproc', 1, 'fid', fid, 'logfid', logfid );
fid = logfid;
elseif( strcmp(opt.solver,'su2') )
logfid = fid; if( ~got.fid ), fid = []; end
fea.sol.u = su2( fea, 'fid', fid, 'logfid', logfid );
fid = logfid;
else
fea.sol.u = solvestat( fea, 'init', init0, 'fid', fid );
end
% Postprocessing.
s_Ma = fea.phys.ee.eqn.vars{end-1,2};
if( opt.iplot>0 )
postplot( fea, 'surfexpr', s_Ma )
title(fea.phys.ee.eqn.vars{end-1,1})
end
% Error checking.
r = evalexprp( fea.dvar{1}, fea );
u = evalexprp( fea.dvar{2}, fea );
v = evalexprp( fea.dvar{3}, fea );
p = evalexprp( fea.dvar{4}, fea );
r_ref = evalexprp( rref, fea );
u_ref = evalexprp( uref, fea );
v_ref = evalexprp( vref, fea );
p_ref = evalexprp( pref, fea );
out.err = [ sum(abs(r_ref-r))/size(fea.grid.p,2), ...
sum(abs(u_ref-u))/size(fea.grid.p,2), ...
sum(abs(v_ref-v))/size(fea.grid.p,2), ...
sum(abs(p_ref-p))/size(fea.grid.p,2) ];
out.pass = all(out.err<opt.tol);
if( nargout==0 )
clear fea out
end