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authorpriyanka2015-06-24 15:03:17 +0530
committerpriyanka2015-06-24 15:03:17 +0530
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+clc
+clear
+
+//input data
+D=0.3 //inner duct diameter in m
+P1=10 //Static pressure at entrance in bar
+T1=400 //Static temperature at entry in Kelvin
+M1=3 //Mach number at entrance
+M2=1 //Mach number at exit
+k=1.3 //Adiabatic constant
+R=287 //Specific Gas constant in J/kg-K, wrong printing in question
+f=0.002 //frictional factor
+
+//calculation
+p1=0.233 //Pressure ratio from gas tables (M=3,k=1.4,isentropic)
+Pt=P1/p1 //Static pressure at entrance in bar
+t1=0.489 //Temperature ratio from gas tables (M=3,k=1.4,isentropic)
+Tt=T1/t1 //Static temperature at entrance in K
+X1=0.628 //frictional constant fanno parameter from gas tables,fanno flow tables @M1,k=1.3
+L1=(X1*D)/(4*f) //Length of the pipe in m
+d_t=(Pt*10^5)/(R*Tt) //Density at critical state in kg/m^3, Pt in Pa
+at=sqrt(k*R*Tt) //Sound velocity in m/s, R in J/kg
+Ct=at //air velocity in m/s
+At=(%pi*D^2)/4 //Critical area in m^2
+m=d_t*At*Ct //Mass flow rate in kg/s
+
+//output
+printf('(A)Length of the pipe is %3.2f m\n (B)Mass flow rate is %3.3f kg/s',L1,m)