% The input conditions of the EVA sim_repeat = 3; % of the times of the simulation repeat filename = 'output1.xlsx'; % the excel data file name must be in this format C_16 = 0.18; % The volume fraction of the fuel %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% A = 4.05; W = 3; Ht = 4; shape = 4; % - 1:Sphere 2:Cylinder 3:Box(sphere) 4:Box(ellipsoid+sphere) vent = 2; % Venting? - 1:Closed 2:Open mass = 1; % Gas venting - 1:Unburnt 2:Burnt R = 2; % Radius L = W; % length of the cylinder Cd = 0.6; % Discharge Coefficient StSl = 2; % Turbulent flame coefficient St/Sl mx = 3; % Flame upper limit: h = 1e-3; % Time step XH20 = 0; % initial mole fraction of H2O Ti = 298; % Initial temperature K Pi = 1.01e5; % initial pressure (Pa)