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| function self = gui_CalculateButtonPushed(app) | ||
| % % Start | ||
| % self.Lamp.Color = 'Yellow'; | ||
| % % self = self(self, self.UITable_P.Data(:, 1)'); | ||
| % self = App(self, 'Soot Formation'); | ||
| % % Get initial parameters | ||
| % self = gui_get_parameters(self); | ||
| % % Constants | ||
| % self.C.l_phi = length(self.PD.phi.value); | ||
| % self.ind_Fuel = strcmp(self.UITable_R.Data(:,4), 'Fuel'); | ||
| % self.ind_Oxidizer = strcmp(self.UITable_R.Data(:,4), 'Oxidant'); | ||
| % self.ind_Inert = strcmp(self.UITable_R.Data(:,4), 'Inert'); | ||
| % % Get Name Reactants species | ||
| % gui_get_reactants(self); | ||
| % for i=self.C.l_phi:-1:1 % Evading preallocate struct | ||
| % if self.flag_PR1; self.PD.TR.value = self.PR1_vector(i); end | ||
| % if self.flag_PR2; self.PD.pR.value = self.PR2_vector(i); end | ||
| % if self.flag_PP1; self.PD.TP.value = self.PP1_vector(i); end | ||
| % if self.flag_PP2; self.PD.pP.value = self.PP2_vector(i); end | ||
| % % Define Fuel | ||
| % self = Define_F(self); | ||
| % % Define Oxidizer | ||
| % self = Define_O(self); | ||
| % % Define Inert | ||
| % self = Define_I(self); | ||
| % % Compute properties | ||
| % self = Define_FOI(self, i); | ||
| % % Solve Problem selected | ||
| % self = SolveProblem(self, i); | ||
| % % Display results command window | ||
| % results(self, i); | ||
| % end | ||
| % self.Lamp.Color = 'Green'; | ||
| % end | ||
|
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||
| % SUB-PASS FUNCTIONS | ||
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| self = App(app, 'Soot formation'); | ||
| %% PROBLEM CONDITIONS | ||
| [self.PD.TR.value, flag_PR1] = gui_get_prop(app, app.PR1.Value, 'TR'); | ||
| [self.PD.pR.value, flag_PR2] = gui_get_prop(app, app.PR2.Value, 'pR'); | ||
| [self.PD.phi.value, flag_phi] = gui_get_prop(app, app.edit_phi.Value, 'phi'); | ||
| %% PROBLEM TYPE | ||
| switch self.PD.ProblemType | ||
| case 'TP' % * TP: Equilibrium composition at defined T and p | ||
| [self.PD.TP.value, flag_PP1] = gui_get_prop(app, app.PP1.Value, 'TP'); | ||
| [self.PD.pP.value, flag_PP2] = gui_get_prop(app, app.PP2.Value, 'pP'); | ||
| case 'HP' % * HP: Adiabatic T and composition at constant p | ||
| self.PD.pP.value = self.PD.pR.value; | ||
| case 'SP' % * SP: Isentropic (i.e., adiabatic) compression/expansion to a specified p | ||
| self.PD.pP.value = 10:1:50; self.PD.phi.value = 1*ones(1, length(self.PD.pP.value)); | ||
| % app.PD.pP.value = 10*ones(1, length(app.PD.phi.value)); | ||
| case 'TV' % * TV: Equilibrium composition at defined T and constant v | ||
| self.PD.TP.value = 2000; | ||
| self.PD.pP.value = self.PD.pR.value; % guess | ||
| case 'EV' % * EV: Equilibrium composition at Adiabatic T and constant v | ||
| self.PD.pP.value = self.PD.pR.value; | ||
| % app.PD.pR.value = logspace(0,2,20); app.PD.phi.value = 1*ones(1,length(app.PD.pR.value)); | ||
| case 'SV' % * SV: Isentropic (i.e., fast adiabatic) compression/expansion to a specified v | ||
| % REMARK! vP_vR > 1 --> expansion, vP_vR < 1 --> compression | ||
| self.PD.vP_vR.value = 0.5:0.01:2; self.PD.phi.value = 1*ones(1, length(self.PD.vP_vR.value)); | ||
| case 'SHOCK_I' % * SHOCK_I: CALCULATE PLANAR INCIDENT SHOCK WAVE | ||
| u1 = logspace(2, 5, 500); | ||
| u1 = u1(u1<20000); u1 = u1(u1>=360); | ||
| % u1 = [356,433,534,658,811,1000,1233,1520,1874,2310,2848,3511,4329,5337,6579,8111,9500,12328,15999,18421,21210,24421,28118,32375,37276,42919,49417,56899,65513]; | ||
| % u1 = linspace(360, 9000, 1000); | ||
| % u1 = 20000; | ||
| self.PD.u1.value = u1; self.PD.phi.value = ones(1,length(self.PD.u1.value)); | ||
| case 'SHOCK_R' % * SHOCK_R: CALCULATE PLANAR POST-REFLECTED SHOCK STATE | ||
| u1 = linspace(400, 6000, 1000); | ||
| % u1 = 2000; | ||
| self.PD.u1.value = u1; self.PD.phi.value = ones(1,length(self.PD.u1.value)); | ||
| case 'DET' % * DET: CALCULATE CHAPMAN-JOUGET STATE (CJ UPPER STATE) | ||
| % app.PD.TR_vector.value = app.PD.TR.value; | ||
| case 'DET_OVERDRIVEN' % * DET_OVERDRIVEN: CALCULATE OVERDRIVEN DETONATION | ||
| self.PD.overdriven.value = 1:0.1:10; self.PD.phi.value = 1*ones(1,length(self.PD.overdriven.value)); | ||
| end | ||
| %% LOOP | ||
| self.C.l_phi = length(self.PD.phi.value); | ||
| tic | ||
| for i=self.C.l_phi:-1:1 | ||
| % DEFINE FUEL | ||
| self.PD.S_Fuel = {'CH4'}; self.PD.N_Fuel = 1; | ||
| self = Define_F(self); | ||
| % DEFINE OXIDIZER | ||
| self.PD.S_Oxidizer = {'O2'}; self.PD.N_Oxidizer = self.PD.phi_t/self.PD.phi.value(i); | ||
| self = Define_O(self); | ||
| % DEFINE DILUENTS/INERTS | ||
| self.PD.proportion_N2_O2 = 79/21; | ||
| self.PD.S_Inert = {'N2'}; self.PD.N_Inert = self.PD.phi_t/self.PD.phi.value(i) * self.PD.proportion_N2_O2; | ||
| self = Define_I(self); | ||
| % COMPUTE PROPERTIES | ||
| self = Define_FOI(self, i); | ||
| % PROBLEM TYPE | ||
| self = SolveProblem(self, i); | ||
| % DISPLAY RESULTS COMMAND WINDOW | ||
| results(self, i); | ||
| end | ||
| toc | ||
| %% DISPLAY RESULTS (PLOTS) | ||
| self.Misc.display_species = {}; | ||
| % app.Misc.display_species = {'CO','CO2','H','HO2','H2','H2O','NO','NO2','N2','O','OH','O2','Cbgrb'}; | ||
| closing(self); | ||
| end |
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