diff options
author | priyanka | 2015-06-24 15:03:17 +0530 |
---|---|---|
committer | priyanka | 2015-06-24 15:03:17 +0530 |
commit | b1f5c3f8d6671b4331cef1dcebdf63b7a43a3a2b (patch) | |
tree | ab291cffc65280e58ac82470ba63fbcca7805165 /1955/CH5/EX5.6/example6.sce | |
download | Scilab-TBC-Uploads-b1f5c3f8d6671b4331cef1dcebdf63b7a43a3a2b.tar.gz Scilab-TBC-Uploads-b1f5c3f8d6671b4331cef1dcebdf63b7a43a3a2b.tar.bz2 Scilab-TBC-Uploads-b1f5c3f8d6671b4331cef1dcebdf63b7a43a3a2b.zip |
initial commit / add all books
Diffstat (limited to '1955/CH5/EX5.6/example6.sce')
-rwxr-xr-x | 1955/CH5/EX5.6/example6.sce | 33 |
1 files changed, 33 insertions, 0 deletions
diff --git a/1955/CH5/EX5.6/example6.sce b/1955/CH5/EX5.6/example6.sce new file mode 100755 index 000000000..3d24ff7a5 --- /dev/null +++ b/1955/CH5/EX5.6/example6.sce @@ -0,0 +1,33 @@ +clc
+clear
+//input data
+R=0.5//Degree of reaction
+P1=14//Initial pressure in bar
+T1=588//Initial temperature in K
+P2=0.14//Final pressure in bar
+Ns=0.75//Stage efficiency
+RF=1.04//Reheat factor
+N=20//No. of stages
+W=11770//Total power output in kW
+a1=20//Exit blade angle in degree
+hD=1/12//Ratio of blade height to blade mean diameter
+
+//calculations
+hs1=3080//Isentropic enthalpy at initial condition from mollier chart in kJ/kg
+hs2=2270//Isentropic enthalpy at final condition from mollier chart in kJ/kg
+dhs=hs1-hs2//Isentropic enthalpy change in kJ/kg
+Nt=Ns*RF//Overall efficiency
+dh=Nt*dhs//Actual enthalpy drop in kJ/kg
+hs=dh/N//Enthalpy drop per stage in kJ/kg
+m=W/dh//Mass flow rate in kg/s
+C11=1.43*1//Velocity of steam at exit from nozzle in m/s in terms of U for 0.5 degree of reaction
+Wm=1*((2*C11*sind(90-a1))-1)//Work done per mass of steam in terms of U^2 in kJ/kg
+U=((hs*10^3)/Wm)^(1/2)//Mean blade velocity in m/s as work done equals enthalpy drop per stage
+C1=1.43*U//Velocity of steam at exit from nozzle in m/s
+Ca=C1*cosd(90-a1)//Flow velocity in m/s
+v=1.618//Specific volume of steam from steam table at 1.05 bar with dry saturated steam in m^3/kg
+D=((m*v)/(hD*3.14*Ca))^(1/2)//Blade mean diameter in m
+N=(U*60)/(3.14*D)//Rotor speed in rpm
+
+//output
+printf('(a)Mass flow rate of steam is %3.2f kg/s\n(b)Mean blade velocity is %3.1f m/s \n(c)Blade mean diameter is %3.3f m \n(d)Rotor speed is %3i rpm',m,U,D,N)
|