Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Notes on this paper
National Examination 07-Mec-A6 — Fluid Machinery, December 2013. Closed book, 3 hours. Section A (Calculative) Q1–Q5, Section B (Descriptive) Q6–Q8; candidates answer four from A and two from B (six of eight, 60 marks). All eight questions are solved as a study resource.
Reference texts: Fox & McDonald, Introduction to Fluid Mechanics (turbomachinery chapter); S.L. Dixon & C.A. Hall, Fluid Mechanics and Thermodynamics of Turbomachinery; R.K. Turton, Principles of Turbomachinery; Cohen, Rogers & Saravanamuttoo, Gas Turbine Theory. Constants used (exam reference sheet): g = 9.81 m/s², ρwater = 1000 kg/m³, Patm = 100 kPa.
Given. The radial-flow impeller geometry, speed and duty are as tabulated below.
Given data
D₁ / D₂
0.130 / 0.300 m
h₁ / h₂
0.020 / 0.010 m
β₁ / β₂
20° / 25°
Speed N
1750 rev/min
Flow Q
0.030 m³/s
Head H
35 m
Find. Blade, radial and whirl velocities at both stations; the shaft torque and power; and the hydraulic power and efficiency.
Inlet: radial water velocity V_r1 = 3.67 m/s, small pre-whirl V_w1 = 1.82 m/s.
Outlet: whirl V_w2 = 20.66 m/s drives the head and torque.
Approach. Blade speed $U=\omega r$; radial velocity from continuity over the cylindrical flow area $\pi D h$; whirl from the blade-angle triangle $\tan\beta=V_r/(U-V_w)$; torque from Euler’s moment-of-momentum, power $T\omega$; efficiency = water power / shaft power.
(b) Radial velocities. Continuity over $A=\pi D h$: $$V_{r1}=\frac{Q}{\pi D_1 h_1}=\frac{0.030}{\pi(0.130)(0.020)}=3.67\ \text{m/s},\quad V_{r2}=\frac{0.030}{\pi(0.300)(0.010)}=3.18\ \text{m/s}$$
(c) Whirl velocities. From $\tan\beta=V_r/(U-V_w)$, i.e. $V_w=U-V_r/\tan\beta$: $$V_{w1}=11.9-\frac{3.67}{\tan20^\circ}=1.8\ \text{m/s},\quad V_{w2}=27.5-\frac{3.18}{\tan25^\circ}=20.7\ \text{m/s}$$
(d) Torque and power. Euler moment of momentum $$T=\rho Q(r_2V_{w2}-r_1V_{w1})=1000\cdot 0.030\,(0.150\cdot 20.7-0.065\cdot 1.8)=\boxed{89.4\ \text{N}\,\text{m}}$$$$P_{shaft}=T\omega=89.4\cdot 183.3=\boxed{16.4\ \text{kW}}$$
(e) Hydraulic power and efficiency. $$P_{hyd}=\rho g Q H=1000\cdot 9.81\cdot 0.030\cdot 35=10.3\ \text{kW}$$$$\eta=\frac{P_{hyd}}{P_{shaft}}=\frac{10.3}{16.4}=\boxed{62.9\%}$$