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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 18.32 IFR turbine stage efficiency
+
+// part(b)
+R=0.48;
+sigma_s=0.6;
+n_n=0.92;
+alpha_2=15; // air angle at nozzle exit(from tangential direction)
+n_st=2*sigma_s*sqrt(n_n*(1-R))*cosd(alpha_2);
+disp("%",n_st*100,"stage efficiency of the radial turbine is")