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 prototype and its homologous model share the design and test data tabulated below.
Given data (prototype / model)
Generator output
120 MW
Net head HP
65 m
Speed NP
125 rev/min
Design flow QP
200 m³/s
Runner dia DP
5.462 m
Model dia DM
0.200 m
Model head HM
10 m
Prototype elec. eff.
98%
Find. Dimensionless specific speed and turbine type; overall efficiency; homologous model speed, flow and ideal power; and the model hydraulic efficiency target via the Moody scale-up.
Approach. Use the reference-sheet dimensionless power specific speed to classify the machine; overall efficiency from output over water power; the similarity groups $gH/N^2D^2$ and $Q/ND^3$ for the model conditions; and the full Moody equation to relate model and prototype hydraulic efficiency.
(a) Specific speed. With $\omega=2\pi N/60=13.09\ \text{rad/s}$, the dimensionless power specific speed is $$\Omega_{sp}=\frac{\omega P^{1/2}}{\rho^{1/2}(gH)^{5/4}}=\frac{13.09\,(120\times10^6)^{1/2}}{1000^{1/2}(9.81\cdot 65)^{5/4}}=\boxed{1.42}$$A value near 1.4 (rad) lies in the Francis range — consistent with the 65 m head.
(b) Overall efficiency. $$\eta_{ov}=\frac{P_{elec}}{\rho g Q_P H_P}=\frac{120\times10^{6}}{1000\cdot 9.81\cdot 200\cdot 65}=\boxed{94.1\%}$$
(c) Model speed. Equal head coefficient $gH/(N^2D^2)$ gives $$N_M=N_P\frac{D_P}{D_M}\sqrt{\frac{H_M}{H_P}}=125\cdot\frac{5.462}{0.200}\sqrt{\frac{10}{65}}=\boxed{1339\ \text{rev/min}}$$
(d) Model flow. Equal flow coefficient $Q/(ND^3)$: $$Q_M=Q_P\frac{N_M}{N_P}\Big(\frac{D_M}{D_P}\Big)^3=200\cdot 10.71\cdot(0.03662)^3=\boxed{0.105\ \text{m}^3/\text{s}}$$
(e) Ideal model power. $$P_M=\rho g Q_M H_M=1000\cdot 9.81\cdot 0.105\cdot 10=\boxed{10.3\ \text{kW}}$$
(f) Model efficiency via Moody. The prototype must reach hydraulic efficiency $\eta_P=\eta_{ov}/\eta_{elec}=0.941/0.98=0.960$. The Moody relationship $\eta_P=1-(1-\eta_M)\left(\tfrac{D_M}{D_P}\right)^{1/4}\left(\tfrac{H_M}{H_P}\right)^{1/10}$ inverts to $$1-\eta_M=\frac{1-\eta_P}{(D_M/D_P)^{1/4}(H_M/H_P)^{1/10}}=\frac{0.0398}{0.363}\Rightarrow \eta_M=\boxed{89.0\%}$$
Check: The exam sheet also lists an approximate Moody form using the diameter ratio only, $(1-\eta_M)/(1-\eta_P)=(D_P/D_M)^{1/5}$, which gives ηM ≈ 92.3%. The full form is used above because the model head (10 m) differs from the prototype (65 m); both are acceptable exam answers if stated.