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+clc
+P1 = 101.3e03
+P4 = P1 // in Pa
+P2 = 8*P1
+P3 = P2
+T1 = 288
+Vs = 2000
+V3 = 100
+Vc = V3
+V1 = Vs + Vc
+n = 1.25
+R = 287
+V4 = ((P3/P4)^(1/n))*V3
+W = ((n*P1*(V1-V4)*1e-06)/(n-1))*(((P2/P1)^((n-1)/n))-1)
+P = (W*800*0.001)/60
+
+m = (P1*(V1-V4)*1e-06)/(R*T1)
+m_dot = m*800
+
+FAD = (V1-V4)*1e-06*800
+
+Wt = P1*(V1-V4)*1e-06*log(P2/P1)
+n_isothermal = (Wt*800*0.001)/(P*60)
+
+Pi = P/0.85
+n_v =100*(V1-V4)/Vs
+printf("\n Example 19.3\n")
+printf("\n Indicated poer is %f kW",P)
+printf("\n Volumetric efficiency is %f percent",n_v)
+printf("\n Mass flow rate is %f kg/min",m_dot)
+printf("\n Free air delivery is %f m^3/min",FAD)
+printf("\n Isothermal efficiency is %f percent",100*n_isothermal)
+printf("\n Input power is %f kW",Pi)
+
+//The answers vary due to round off error
+