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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
+P=8//Power in MW
+N=5000//Speed in rpm
+p=40//pressure in bar
+T=500//Temperature in degree C
+p2=0.1//Pressure in bar
+in=0.85//Internal efficiency of turbine
+nm=0.96//Mechanical efficiency
+nn=0.92//Nozzle efficiency
+a=15//Nozzle angle in degrees
+Vb=300//Blade velocity in m/s
+
+//Calculations
+V1=(2*Vb)/cosd(a)//Velocity in m/s
+dh=((V1/44.72)^2/nn)//Change in enthalpy in kJ/kg
+h1=3445.3//Enthalpy in kJ/kg
+s1=7.0901//Entropy in kJ/kg.K
+s2=s1//Entropy in kJ/kg.K
+x2=(s2-0.6493)/7.5009//Dryness fraction
+h2s=(191.83+x2*2392.8)//Enthalpy in kJ/kg
+h12s=(h1-h2s)//Change in enthalpy in kJ/kg
+n=(h12s/dh)//Number of stages
+w=((P*1000)/(in*nm))/h12s//Mass flow rate in kg/s
+h13=(nn*dh)//Change in enthalpy in kJ/kg
+h3=h1-h13//Enthalpy in kJ/kg
+v3=0.17//Specific volume in m^3/kg
+A=(w*v3)/V1//Area in m^2
+hm=(A/(((Vb*60)/N)*sind(a)))*1000//Height in mm
+
+//Output
+printf('(a) the number of impulse stages are%3.0f \n (b) the nozzle height is %3.1f mm',n,hm)