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Dave Goodwin 2003-06-09 06:49:52 +00:00
parent 7fb8532914
commit 73c0907c59
1 changed files with 41 additions and 41 deletions
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Cantera/matlab/cantera/examples/flame2.m
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@ -1,6 +1,6 @@
%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
%
% A burner-stabilized flat flame
% An axisymmetric stagnation-point non-premixed flame
%
%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
@ -8,18 +8,19 @@ t0 = cputime; % record the starting time
% parameter values
p = 0.05*oneatm; % pressure
tburner = 373.0; % burner temperature
mdot = 0.04; % kg/m^2/s
p = oneatm; % pressure
tin = 300.0; % inlet temperature
mdot_o = 0.24; % air, kg/m^2/s
mdot_f = 0.08; % fuel, kg/m^2/s
rxnmech = 'gri30.xml'; % reaction mechanism file
transport = 'Mix'; % transport model
comp = 'O2:0.21, N2:0.78, AR:0.01'; % premixed gas composition
comp2 = 'C2H2:1'; % premixed gas composition
comp1 = 'O2:0.21, N2:0.78, AR:0.01'; % air composition
comp2 = 'C2H6:1'; % fuel composition
initial_grid = [0.0 0.02 0.04 0.06 0.08 0.1 0.12 0.14 0.16 0.18 0.2]; % m
initial_grid = 0.02*[0.0 0.2 0.4 0.6 0.8 1.0]; % m
tol_ss = [1.0e-7 1.0e-12]; % [rtol atol] for steady-state
tol_ss = [1.0e-5 1.0e-12]; % [rtol atol] for steady-state
% problem
tol_ts = [1.0e-3 1.0e-4]; % [rtol atol] for time stepping
@ -37,8 +38,8 @@ refine_grid = 1; % 1 to enable refinement, 0 to
%
gas = IdealGasMix(rxnmech, transport);
% set its state to that of the unburned gas at the burner
set(gas,'T', tburner, 'P', p, 'X', comp);
% set its state to that of the fuel (arbitrary)
set(gas,'T', tin, 'P', p, 'X', comp2);
@ -51,40 +52,36 @@ set(f, 'tol', tol_ss, 'tol-time', tol_ts);
%%%%%%%%%%%%%%% create the burner %%%%%%%%%%%%%%%%%%%%%%%%%%%%%
%%%%%%%%%%%%%%% create the air inlet %%%%%%%%%%%%%%%%%%%%%%%%%%%%%
%
% The burner is an Inlet object. The temperature, mass flux,
% and composition (relative molar) may be specified.
% The temperature, mass flux, and composition (relative molar) may be
% specified.
%
burner = Inlet('burner');
set(burner, 'T', tburner, 'MassFlux', mdot, 'X', comp);
inlet_o = Inlet('air_inlet');
set(inlet_o, 'T', tin, 'MassFlux', mdot_o, 'X', comp1);
%%%%%%%%%%%%%% create the outlet %%%%%%%%%%%%%%%%%%%%%%%%%%%%
%%%%%%%%%%%%%% create the fuel inlet %%%%%%%%%%%%%%%%%%%%%%%%%%%%
%
% The type of flame is determined by the object that terminates
% the domain. An Outlet object imposes zero gradient boundary
% conditions for the temperature and mass fractions, and zero
% radial velocity and radial pressure gradient.
%
s = Inlet('right');
set(s, 'T', tburner, 'MassFlux', 0.04, 'X', comp2);
inlet_f = Inlet('fuel_inlet');
set(inlet_f, 'T', tin, 'MassFlux', mdot_f, 'X', comp2);
%%%%%%%%%%%%% create the flame object %%%%%%%%%%%%
%
% Once the component parts have been created, they can be assembled
% to create the flame object.
%
fl = flame(gas, burner, f, s);
fl = flame(gas, inlet_o, f, inlet_f);
% if the starting solution is to be read from a previously-saved
% solution, uncomment this line and edit the file name and solution id.
%restore(fl,'h2flame2.xml', 'energy')
resid(fl, 'flow')
solve(fl, 1, 1);
% solve with fixed temperature profile first
solve(fl, loglevel, refine_grid);
%%%%%%%%%%%% enable the energy equation %%%%%%%%%%%%%%%%%%%%%
@ -95,10 +92,9 @@ solve(fl, 1, 1);
%
enableEnergy(f);
resid(fl, 'flow')
setRefineCriteria(fl, 2, 200.0, 0.1, 0.1);
solve(fl, 1, 1);
saveSoln(fl,'h2fl.xml','energy',['solution with energy' ...
solve(fl, loglevel, refine_grid);
saveSoln(fl,'c2h6.xml','energy',['solution with energy' ...
' equation']);
@ -112,20 +108,24 @@ disp(e);
%%%%%%%%%% make plots %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
figure(1);
subplot(2,2,1);
subplot(2,3,1);
plotSolution(fl, 'flow', 'T');
title('Temperature [K]');
subplot(2,2,2);
plotSolution(fl, 'flow', 'H2O');
title('Axial Velocity [m/s]');
subplot(2,2,3);
subplot(2,3,2);
plotSolution(fl, 'flow', 'C2H6');
title('C2H6 Mass Fraction');
subplot(2,3,3);
plotSolution(fl, 'flow', 'O2');
title('O2 Mass Fraction');
subplot(2,2,4);
plotSolution(fl, 'flow', 'H2');
title('H2 Mass Fraction');
%subplot(2,2,4);
%plotSolution(fl, 'flow', 'V');
%title('V');
subplot(2,3,4);
plotSolution(fl, 'flow', 'CH');
title('CH Mass Fraction');
subplot(2,3,5);
plotSolution(fl, 'flow', 'V');
title('Radial Velocity / Radius [s^-1]');
subplot(2,3,6);
plotSolution(fl, 'flow', 'u');
title('Axial Velocity [m/s]');