Add: example HP multicomponent fuel

examples/Example_HP_NATURAL_GAS.m

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+% -------------------------------------------------------------------------
+% EXAMPLE: HP_NATURAL_GAS
+%
+% Compute adiabatic temperature and equilibrium composition at constant
+% pressure (e.g., 1.01325 bar) for lean to rich natural gas (0.85% CH4, ...
+% 0.10% C2H6, 0.0035% CO2)-air mixtures at standard conditions, a set of
+% 24 species considered and a set of equivalence ratios phi contained in
+% (0.5, 5) [-]
+%   
+% 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 July 22 2022
+% -------------------------------------------------------------------------
+
+%% INITIALIZE
+self = App('Soot formation');
+%% INITIAL CONDITIONS
+self = set_prop(self, 'TR', 300, 'pR', 1 * 1.01325, 'phi', 0.5:0.01:5);
+self.PD.S_Fuel     = {'CH4', 'C2H6', 'CO2'};
+self.PD.N_Fuel     = [0.85, 0.1, 0.0035];
+self.PD.S_Oxidizer = {'N2', 'O2', 'Ar', 'CO2'};
+self.PD.ratio_oxidizers_O2 = [78.084, 20.9476, 0.9365, 0.0319] ./ 20.9476;
+%% ADDITIONAL INPUTS (DEPENDS OF THE PROBLEM SELECTED)
+self = set_prop(self, 'pP', self.PD.pR.value); 
+%% SOLVE PROBLEM
+self = solve_problem(self, 'HP');
+%% DISPLAY RESULTS (PLOTS)
+post_results(self);