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22-Mec-A6 Fluid Machinery · December 2013

Question 2 of 8: Hydro Turbine Model

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.

Question 2: Hydro Turbine Model (10 marks)

Question text not reproduced: the examination questions are © Engineers and Geoscientists BC. Open the official past paper (linked at the top of this page) to read the question, then follow the worked solution below.

Given. The prototype and its homologous model share the design and test data tabulated below.

Given data (prototype / model)
Generator output120 MWNet head HP65 m
Speed NP125 rev/minDesign flow QP200 m³/s
Runner dia DP5.462 mModel dia DM0.200 m
Model head HM10 mPrototype 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.

  1. (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.
  2. (b) Overall efficiency. $$\eta_{ov}=\frac{P_{elec}}{\rho g Q_P H_P}=\frac{120\times10^{6}}{1000\cdot 9.81\cdot 200\cdot 65}=\boxed{94.1\%}$$
  3. (c) Model speed. Equal head coefficient $gH/(N^2D^2)$ gives $$N_M=N_P\frac{D_P}{D_M}\sqrt{\frac{H_M}{H_P}}=125\cdot\frac{5.462}{0.200}\sqrt{\frac{10}{65}}=\boxed{1339\ \text{rev/min}}$$
  4. (d) Model flow. Equal flow coefficient $Q/(ND^3)$: $$Q_M=Q_P\frac{N_M}{N_P}\Big(\frac{D_M}{D_P}\Big)^3=200\cdot 10.71\cdot(0.03662)^3=\boxed{0.105\ \text{m}^3/\text{s}}$$
  5. (e) Ideal model power. $$P_M=\rho g Q_M H_M=1000\cdot 9.81\cdot 0.105\cdot 10=\boxed{10.3\ \text{kW}}$$
  6. (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.
Question 2 results
QuantityValue
(a) Specific speed / typeΩsp = 1.42 → Francis
(b) Overall efficiency94.1%
(c) Model speed1339 rev/min
(d) Model flow0.105 m³/s
(e) Model ideal power10.3 kW
(f) Required model efficiency89.0% (full Moody)