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Diffstat (limited to '3831/CH15/EX15.3/Ex15_3.sce')
-rw-r--r-- | 3831/CH15/EX15.3/Ex15_3.sce | 37 |
1 files changed, 37 insertions, 0 deletions
diff --git a/3831/CH15/EX15.3/Ex15_3.sce b/3831/CH15/EX15.3/Ex15_3.sce new file mode 100644 index 000000000..4d5c1036a --- /dev/null +++ b/3831/CH15/EX15.3/Ex15_3.sce @@ -0,0 +1,37 @@ +// Example 15_3
+clc;funcprot(0);
+// Given data
+T=20.0;// °C
+CO_2=7.10;// %
+CO=0.800;// %
+O_2=9.90;// %
+N_2=82.2;// %
+M_air=28.97;// lbmdry air/lbmole dry air
+
+// Solution
+// (a)
+n=7.10+0.800;// Carbon (C) balance
+// m=2*b
+a=82.2/3.76;// Nitrogen (N2) balance
+b=2*(a-(7.10+(0.800/2)+9.90));// Oxygen (O2) balance
+m=2*b;// Hydrogen (H) balance
+printf("\n(a)The hydrocarbon model (CnHm) of the fuel is C_%1.2fH_%2.0f",n,m);
+// (b)
+M_fuel=(7.90*(12))+(18.0*(1));// lbm/lbmole
+Fc_C=7.90*12.0*113;// lbm C/lbm fuel
+Fc_H=((9.00)*(2.016))/113;// lbmH/lbmfuel
+printf("\n(b)The molecular mass of the fuel in this model,M_fuel=%3.0f lbm/lbmole \n The fuel’s composition on a mass basis is %0.3f lbmC/lbmfuel and %0.3f lbmH/lbm fuel",M_fuel,Fc_C,Fc_H);
+// (c)
+n_air=21.9*(1+3.76);// The stoichiometric coefficient of the reaction
+n_fuel=1;// The stoichiometric coefficient of the reaction
+AF_molar=n_air/n_fuel;// moles air/mole fuel
+AF_mass=AF_molar*(28.97/(M_fuel));// lbm air/lbm fuel
+printf("\n(c)The air-fuel ratio on a molar and a mass basis,(A/F)_molar=%3.0f moles air/molefuel and (A/F)_mass=%2.1f lbm air/lbm fuel",AF_molar,AF_mass);
+// (d)
+b=7.90;// Carbon (C) balance
+c=18.0;// Hydrogen (H) balance
+a=b+(c/2);// Oxygen (O2) balance
+d=3.76*a;// Nitrogen (N2) balance
+AF_mt=(12.4*(1+3.76))/1;// mole air/mole fuel
+per_ta=(AF_molar/AF_mt)*100;// The percent of theoretical air used in the actual combustion process (%)
+printf("\n(d)The percentage of theoretical air used in the combustion process,Percentage of theoritical air=%3.0f percentage or %2.0f percentage excess air",per_ta,(per_ta-100));
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