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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=800//Diameter in mm
+N=3000//Speed in rpm
+V1=300//Velocity in m/s
+a=20//Nozzle angle in degrees
+f=0.86//Frictional factor
+T=140//Axial thrust in N
+
+//Calculations
+Vb=((3.14*(d/1000)*N)/60)//Velocity in m/s
+b1=atand((V1*sind(a))/((V1*cosd(a))-Vb))//Blade angle in degrees
+b2=b1//Blade angle in degrees
+Vr1=(V1*sind(a))/sind(b1)//Velocity in m/s
+Vr2=f*Vr1//Velocity in m/s
+w=(T/((Vr1*sind(b1))-(Vr2*sind(b2))))//Mass flow rate in kg/s
+dVw=(Vr2*cosd(b2))+(Vr1*cosd(b1))//Velocity in m/s
+P=(w*dVw*Vb*10^-3)//Power developed in kW
+
+//Output
+printf('Power deveoped in the blading is %3.2f kW',P)