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authorpriyanka2015-06-24 15:03:17 +0530
committerpriyanka2015-06-24 15:03:17 +0530
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+// scilab Code Exa 18.38 Kaplan turbine 70 rpm
+
+//part(a)flow rate and specific speed
+P=8e3; // Gas Power Output in kW
+N=70; // Speed in RPM
+H=10; // net head in m
+n_m=0.85; // efficiency
+omega=%pi*2*N/60;
+NS=omega*sqrt(P*10e2)*(H^(-5/4))/549.016;
+disp(NS,"(a)the specific speed of turbine is")
+rho=1000; // density in kg/m3
+g=9.81; // gravitational acceleration in m/s2
+Q=P*1e3/(n_m*rho*g*H);
+disp("m3/s",Q,"and the flow rate is")
+
+// part(b) determining the speed, flow rate and power for the model
+Dp_m=12; // Dp_m=Dp/Dm
+Np=N; // Speed for prototype
+Hm=3; // head of the model
+Hp=H; // head for prototype
+Nm=Np*Dp_m*sqrt(Hm/Hp);
+disp("rpm",Nm,"(b)speed for the model is")
+Dm_p=1/Dp_m;
+Qp=Q;
+Qm=(Dm_p^2)*sqrt(Hm/Hp)*Qp;
+disp("m3/s",Qm,"the flow rate for model is")
+Pm=n_m*rho*g*Qm*Hm;
+disp("kW",Pm*1e-3,"the power for the model is")