diff options
Diffstat (limited to '3751/CH6/EX6.8/Ex6_8.sce')
-rw-r--r-- | 3751/CH6/EX6.8/Ex6_8.sce | 37 |
1 files changed, 37 insertions, 0 deletions
diff --git a/3751/CH6/EX6.8/Ex6_8.sce b/3751/CH6/EX6.8/Ex6_8.sce new file mode 100644 index 000000000..43cc49b71 --- /dev/null +++ b/3751/CH6/EX6.8/Ex6_8.sce @@ -0,0 +1,37 @@ +//Fluid System By Shiv Kumar
+//Chapter 6 - Kaplan and Propeller Turbines
+//Example 6.8
+//To Find Inlet and outlet Angles of the Runner blades
+
+clc
+clear
+
+//Given:
+ H=25; //Head, m
+ P=23000; //Shaft Power, KW
+ D=5; //External Diameter of Runner, m
+ d=3; //Diameter of Hub, m
+ N=60; //Rotational Speed, rpm
+ eta_H=95/100; //Hydraulic Efficiency
+ eta_0=88/100; //Overall Efficiency
+ Vw=0; //As there is no exit whirl
+
+//Data Required:
+ rho=1000; //Density of Water, Kg/m^3
+ g=9.81; //Acceleration due to gravity, m/s^2
+
+//Computations
+ Dm=(D+d)/2; //Mean Diameter of Runner, m
+ ui=%pi*Dm*N/60 //m/s
+ Q=P*10^3/(rho*g*H*eta_0); //Discharge, m^3/s
+ Vfi=Q/((%pi/4)*(D^2-d^2)) // m/s
+ Vwi=eta_H*g*H/ui; //m/s
+ uo=ui;
+ Vfo=Vfi;
+ Beta_i=atand(Vfi/(Vwi-ui)); //Degrees
+ Beta_o=atand(Vfo/uo); //Degrees
+
+//Results
+ printf("At the Mean Radius\n\t")
+ printf("Runner Blade Angle at Inlet, Beta_i=%.2f Degrees\n\t",Beta_i) //The answer vary due to round off error
+ printf("Runner Blade Angle at Outlet, Beta_o=%.2f Degrees\n",Beta_o) //The answer vary due to round off error
|