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authorpriyanka2015-06-24 15:03:17 +0530
committerpriyanka2015-06-24 15:03:17 +0530
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+// scilab Code Exa 2.3 Calculation on a compressor
+p1=1.0; // Initial Pressure in bar
+t1=40; // Initial Temperature in degree C
+T1=t1+273; // in Kelvin
+s=8; // number of stages
+m=50; // mass flow rate through the compressor in kg/s
+pr=1.35; // equal Pressure Ratio in each stage
+opr=pr^s; // Overall Pressure Ratio
+gamma=1.4; // Specific Heat Ratio
+cp=1.005; // Specific Heat at Constant Pressure in kJ/(kgK)
+n=0.82; // Overall Efficiency
+
+// part(a) Determining state of air at the compressor exit
+p9=opr*p1;
+delTc=T1*(opr^((gamma-1)/gamma)-1)/n;
+T9=T1+delTc;
+disp("bar",p9,"(a)Exit Pressure is")
+disp("K",T9,"and Exit Temperature is")
+
+// part(b) Determining the polytropic or small stage efficiency
+n_p=((gamma-1)/gamma)*((log(p9/p1))/(log(T9/T1)));
+disp("%",n_p*100,"(b)small stage Efficiency or polytropic efficiency of the compressor is")
+
+// part(c) Determining efficiency of each stage
+n_st=(pr^((gamma-1)/gamma)-1)/(pr^(((gamma-1)/gamma)/n_p)-1);
+disp ("%",n_st*100,"(c)Efficiency of each stage is")
+
+// part(d) Determining power required to drive the compressor
+n_d=0.9; // Overall efficiency of the drive
+P=m*cp*delTc/n_d;
+disp ("MW" ,P/1e3,"(d)Power required to drive the compressor is")