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Diffstat (limited to '3685/CH19/EX19.22/Ex19_22.sce')
-rw-r--r-- | 3685/CH19/EX19.22/Ex19_22.sce | 26 |
1 files changed, 26 insertions, 0 deletions
diff --git a/3685/CH19/EX19.22/Ex19_22.sce b/3685/CH19/EX19.22/Ex19_22.sce new file mode 100644 index 000000000..a86de067f --- /dev/null +++ b/3685/CH19/EX19.22/Ex19_22.sce @@ -0,0 +1,26 @@ +clc
+// Given that
+D = 0.5 // Mean diameter of impeller in m
+N = 15000 // Speed in RPM
+Vf = 230 // Velocity of flow in m/s
+p1 = 1 // Inlet pressure in bar
+T1 = 300 // Inlet temperature in K
+Vw1 = 80 // Velocity of whirl at inlet in m/s
+n_s = 0.88 // Stage efficiency
+rp = 1.5 // Pressure ratio
+gama = 1.4
+cp = 1.0005
+printf("\n Example 19.22\n")
+Vb = (%pi*D*N/60)
+Ts = T1*((rp)^((gama-1)/gama))
+T = T1 + (Ts-T1)/n_s
+Wc = cp*(T-T1)
+Vw2 = Vw1 + (Wc*1000)/(Vb)
+beta1 = atand(Vf/(Vb-Vw1))
+beta2 = atand(Vf/(Vb-Vw2))
+theta = beta2-beta1
+R = 1-((Vw1+Vw2)/(2*Vb))
+
+printf("\n Fluid deflection angle = %f degree,\n Power input = %f kJ/kg,\n The degree of reaction = %d percent",theta,Wc,R*100)
+// The answers given in the book vary because of round off error
+
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