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+// Example 9_2
+clc;funcprot(0);
+// Given data
+m=20;// The mass flow rate of air in kg/min
+P_4=1600;// kPa
+T_1=20+273;// K
+P_1=100;// kPa
+n=0.90;// The efficiency of the compressor
+c_p=1.00;// kJ/kg.K
+k=1.4;// The specific heat ratio
+
+// Calculation
+P_2=sqrt(P_1*P_4);// kPa
+T_3=T_1;// K
+T_2a=T_1*(P_2/P_1)^((k-1)/k);// K
+// Assume T_2'=T_2a
+// P_4/P_3=P_2/P_1
+T_4a=T_3*(P_2/P_1)^((k-1)/k);// K
+T_2=T_1+((1/n)*(T_2a-T_1));// K
+T_4=T_2;// K
+W_comp=((m/60)*c_p*(T_2-T_1))+((m/60)*c_p*(T_4-T_3));// The required power in kW
+printf("\nThe power required to drive the two-stage adiabatic compressor,W_comp=%3.0f kW",W_comp);