22-Mec-A6 Fluid Machinery · May 2014
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Paper format. National Examination 07-Mec-A6-1 Fluid Machinery (May 2014) — closed book, three hours, 60 marks. Section A is calculative (Q1–Q5) and Section B is descriptive (Q6–Q8); the rubric asks for four of Section A plus two of Section B (six questions, each of equal value, 10 marks). All eight questions are solved in full as a study resource. General constants supplied with the paper: g = 9.81 m/s², patm = 100 kPa, pvapour = 2.34 kPa (20 °C), ρwater = 1000 kg/m³, ρair = 1.21 kg/m³ (15 °C), cp,air = 1.005, cv,air = 0.718 kJ/kg·K.
Reference texts. S. L. Dixon & C. A. Hall, Fluid Mechanics and Thermodynamics of Turbomachinery (7th ed.); R. K. Turton, Principles of Turbomachinery; H. Cohen, G. F. C. Rogers & H. I. H. Saravanamuttoo, Gas Turbine Theory (for the axial compressor stage); R. W. Fox, A. T. McDonald & P. J. Pritchard, Introduction to Fluid Mechanics (pump energy equation and affinity laws).
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. Net head Hnet = 1118 ft = 340.8 m; gross head 1226 ft = 373.7 m; P = 62 000 HP = 46.25 MW; N = 300 rev/min; pitch diameter D = 95 in = 2.413 m.
Find. (a) blade-to-jet speed ratio U/V, (b) its deviation from the ideal 0.5, (c) the flow rate.
Approach. The wheel speed follows from the pitch diameter and rpm; the anticipated jet speed follows from the net head via $V=\sqrt{2gH}$; the flow follows from the hydraulic power $P=\rho g Q H_{net}$.
Check: Part I(c) assumes ideal (100%) conversion of net-head energy. A real Pelton unit at ≈ 85% overall efficiency would pass roughly 16.3 m³/s for the same 46.25 MW; the ideal figure is what the stated data supports directly.
Given. P = 120 MW, N = 125 rev/min, H = 65 m, water. (The 217 m³/s, 7 m casing and 5462 mm runner size the machine but are not needed for the dimensionless specific speed.)
Find. (a) power specific speed Ωsp, (b) Thoma σ from the chart, (c) maximum runner elevation Δz above the tailrace.
[Figure not reproduced: Critical-cavitation chart (page 12), redrawn from the printed log–log attachment. The operating point Ω sp = 1.41 lands on the Francis line at σ c ≈ 0.22. The Francis line runs only from about Ω sp = 0.35 to 2.05 and the Kaplan line begins near 1.49, so the two overlap between roughly 1.5 and 2.0 wi. See the official exam paper.]
Approach. Compute the non-dimensional power specific speed, read the critical σ off the Francis curve, then invert the Thoma definition for the permissible runner height.
Check: Δz is sensitive to the graphical read of σc — each 0.01 of reading error moves the setting by 0.65 m, so σc = 0.21 gives −3.7 m and σc = 0.23 gives −5.0 m. Quote the result as roughly 4–5 m of submergence rather than to the centimetre. The sign is robust: σcH exceeds the 9.96 m atmospheric–vapour head by a wide margin, so no plausible read of the Francis line puts this runner above the tailrace.
| Quantity | Value |
|---|---|
| Part I(a): U/V ratio | 0.464 |
| Part I(b): deviation from 0.5 | 7.3 % (friction / nozzle coefficient) |
| Part I(c): flow rate (ideal) | 13.8 m³/s |
| Part II(a): power specific speed Ωsp | 1.41 (Francis) |
| Part II(b): Thoma σc | ≈ 0.22 (Francis line) |
| Part II(c): runner setting Δz | ≈ −4.3 m (4.3 m below tailrace) |