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+clc;
+T01=27+273; // Inlet temperature in kelvin
+p01=1; // Inlet pressure in bar
+rp=3; // Pressure ratio
+Cpa=1.005;// Specific heat of air at constant pressure in kJ/kg K
+Cpg=1.147;// Specific heat of fuel at constant pressure in kJ/kg K
+rg=1.33;// Specific heat ratio of fuel
+r=1.4; // Specific heat ratio of air
+R=287; // Characteristic constant in J/kg K
+
+T_02=T01*rp^((r-1)/r);
+// Turbines 70 years ago
+eff_c=0.65; // Compressor efficiency
+eff_T=0.7; // Turbine efficiency
+T03=700+273; // in kelvin
+T02=T01*(1+((rp^((r-1)/r)-1)/eff_c));
+T04=T03*(1-eff_T*(1-(1/rp^((rg-1)/rg))));
+eff_th=(Cpg*(T03-T04)-Cpa*(T02-T01))/(Cpg*(T03-T02));
+WR=(Cpg*(T03-T04)-Cpa*(T02-T01))/(Cpg*(T03-T04));
+
+disp (WR,"Work ratio = ",eff_th*100,"The Efficiency = ","(i).70 years ago");
+
+//Modern turbines
+eff_c=0.85; // Compressor efficiency
+eff_T=0.9; // Turbine efficiency
+T03=1000+273; // in kelvin
+T02=T01+(T_02-T01)/eff_c;
+T_04=T03/rp^((rg-1)/rg);
+T04=T03-eff_T*(T03-T_04);
+Wc=Cpa*(T02-T01);
+WT=Cpg*(T03-T04);
+WN=WT-Wc;
+eff_th=WN/(Cpg*(T03-T02));
+WR=WN/WT;
+
+disp (WR,"Work ratio = ","%",eff_th*100,"The Efficiency = ","(ii).Modern turbines");