Solve: bug species reverse

examples/Example_ROCKET_IAC_2.m

@@ -2,30 +2,31 @@
 % EXAMPLE: ROCKET Propellants considering an Infinite-Area-Chamber (IAC)
 %
 % Compute rocket propellant performance considering an Infinite-Area-Chamber
-% for lean to rich MON25-MHF3 mixtures at 101.325 bar, a set of 24 species
+% for lean to rich MHF3-MON25 mixtures at 101.325 bar, a set of 24 species
 % considered, a set of equivalence ratios phi contained in (2, 5) [-], and
 % an exit area ratio A_exit/A_throat = 3 
 %   
-% HYDROGEN_L == {'H','H2O','OH','H2','O','O3','O2','HO2','H2O2',...
-%                'H2bLb','O2bLb'}
+% Soot formation == {'CO2','CO','H2O','H2','O2','N2','Ar','Cbgrb',...
+%                    'C2','C2H4','CH','CH3','CH4','CN','H',...
+%                    'HCN','HCO','N','NH','NH2','NH3','NO','O','OH'}
 %   
 % See wiki or list_species() for more predefined sets of species
 %
 % @author: Alberto Cuadra Lara
 %          PhD Candidate - Group Fluid Mechanics
 %          Universidad Carlos III de Madrid
 %                 
-% Last update Jul 30 2022
+% Last update Feb 08 2024
 % -------------------------------------------------------------------------
 
 %% INITIALIZE
 self = App('Soot Formation');
 %% INITIAL CONDITIONS
 self = set_prop(self, 'TR', 298.15, 'pR', 100 * 1.01325, 'phi', 2);
-self.PD.S_Fuel     = {'N2O4bLb', 'N2O3'};
-self.PD.N_Fuel     = convert_weight_percentage_to_moles(self.PD.S_Fuel, [36.67, 63.33], self.DB);
-self.PD.S_Oxidizer = {'CH6N2bLb', 'N2H4bLb'};
-self.PD.wt_ratio_oxidizers = [86, 14];
+self.PD.S_Fuel     = {'CH6N2bLb', 'N2H4bLb'};
+self.PD.N_Fuel     = convert_weight_percentage_to_moles(self.PD.S_Fuel, [86, 14], self.DB);
+self.PD.S_Oxidizer = {'N2O4bLb', 'N2O3'};
+self.PD.wt_ratio_oxidizers = [36.67, 63.33];
 self.PD.FLAG_IAC = true;
 %% ADDITIONAL INPUTS (DEPENDS OF THE PROBLEM SELECTED)
 self = set_prop(self, 'Aratio', 3);