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22-Mec-B6 Advanced Fluid Mechanics · December 2013

Question 1 of 7: Question 1 (Part A, Question A1): Scaling a Fan — Flow, Pressure Rise and Shaft Power at a New Size, Speed and Air Density

Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)

Notes on this paper

Paper format. National Exams, December 2013 — 07-Mec-B6 Advanced Fluid Mechanics. Three hours, open book, any non-communicating calculator permitted. Part A holds four questions weighted 16 marks each (48 per cent of the paper) and Part B three questions weighted 26 marks each (52 per cent); the candidate answers any three in Part A and any two in Part B. All seven questions are worked here. The paper supplies a four-page aid sheet (compressible-flow and shock relations, the boundary-layer integral equations, the Navier–Stokes equations in Cartesian and cylindrical-polar form, and the potential-flow stream and potential functions); every relation quoted below is taken from that sheet, so the arithmetic matches what a candidate had in front of them.

Reference texts.

Conventions used throughout. Air is treated as a perfect gas with γ = 1.4 and R = 287 J/kg·K except where a question names another gas. Pressure conversions use 1 mm Hg = 133.322 Pa and 1 mm H2O = 9.80665 Pa. Compressible-flow ratios are evaluated from the closed-form aid-sheet relations rather than read off a table, so the third significant figure is exact rather than interpolated.

Question 1 (Part A, Question A1): Scaling a Fan — Flow, Pressure Rise and Shaft Power at a New Size, Speed and Air Density (16 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.

QuantityTested fan (state 1) Similar fan (state 2)
Impeller diameterD1 = 0.4 mD2 = 1.0 m
Rotational speedN1 = 970 rpmN2 = 500 rpm
Air temperatureT1 = 10 °C = 283.15 KT2 = 16 °C = 289.15 K
Barometric pressurep1 = 772 mm Hg = 102.925 kPap2 = 760 mm Hg = 101.325 kPa
Volume flow rateQ1 = 0.7 m3/sto be found
Fan total pressureΔp1 = 25 mm H2O = 245.17 Pato be found
Shaft powerP1 = 250 Wto be found
Efficiencyunchanged between the two machines

Find. The volume flow rate, fan total pressure and shaft power delivered by the 1 m fan at 500 rpm in the second air state.

D = 0.4 m, N = 970 rpmQ = 0.7 m3/s, Δp = 25 mm H2Oshaft power = 250 W10 °C, 772 mm HgD = 1.0 m, N = 500 rpmQ = ?, Δp = ?, power = ?16 °C, 760 mm Hggeometrically similar,same efficiencyFan similarity: matched flow, head and power coefficients
Figure A1 — The two geometrically similar fans. Similarity fixes the flow, head and power coefficients; only the density ratio couples the two air states.

Approach. Geometric similarity plus unchanged efficiency means the three dimensionless turbomachine coefficients — flow, head (pressure) and power — take the same value in both machines, so each dimensional quantity scales as a fixed power of the speed ratio, the diameter ratio and (for pressure and power) the air-density ratio, which must first be computed from the two barometric states.

  1. Fix the air density in each state from the perfect-gas law. The two barometric readings convert to absolute pressures, and $$\rho=\frac{p}{RT},\qquad R_{\text{air}}=287\ \text{J/kg}\cdot\text{K}.$$ For the test state, $p_1=772\times133.322=102\,925\ \text{Pa}$ and $T_1=283.15\ \text{K}$, so $\rho_1=102\,925/(287\times283.15)=1.2665\ \text{kg/m}^3$. For the second state, $p_2=760\times133.322=101\,325\ \text{Pa}$ and $T_2=289.15\ \text{K}$, giving $\rho_2=101\,325/(287\times289.15)=1.2210\ \text{kg/m}^3$. The density ratio that carries through the rest of the question is $$\boxed{\ \frac{\rho_2}{\rho_1}=\frac{1.2210}{1.2665}=0.9640\ }$$ — the second fan handles air that is 3.6 per cent lighter, partly because it is warmer and partly because the barometer is lower.
  2. Write the three similarity coefficients. For a family of geometrically similar fans operating at the same efficiency, dimensional analysis (White Ch. 11) gives three groups that must match: $$\begin{aligned} \text{flow coefficient}\quad \phi&=\frac{Q}{ND^{3}}\\ \text{head coefficient}\quad \psi&=\frac{\Delta p}{\rho N^{2}D^{2}}\\ \text{power coefficient}\quad \Pi_P&=\frac{P}{\rho N^{3}D^{5}} \end{aligned}$$ Note that the flow coefficient contains no density: volume flow scales purely kinematically, whereas pressure rise and power both carry one power of density because they are momentum and energy quantities. Because the speed appears only as a ratio, $N$ may be left in rpm throughout provided the same unit is used top and bottom.
  3. Scale the volume flow rate. Equating flow coefficients, $$Q_2=Q_1\left(\frac{N_2}{N_1}\right)\left(\frac{D_2}{D_1}\right)^{3} =0.7\times\frac{500}{970}\times\left(\frac{1.0}{0.4}\right)^{3} =0.7\times0.51546\times15.625.$$ The larger fan turns almost half as fast but sweeps a volume nearly sixteen times larger, and the size term wins decisively: $$\boxed{\ Q_2=5.64\ \text{m}^3/\text{s}\ }$$
  4. Scale the fan total pressure. Equating head coefficients and carrying the density ratio, $$\Delta p_2=\Delta p_1\left(\frac{\rho_2}{\rho_1}\right) \left(\frac{N_2}{N_1}\right)^{2}\left(\frac{D_2}{D_1}\right)^{2} =245.17\times0.9640\times0.26570\times6.2500.$$ Here the speed and size effects nearly cancel — the tip speed $\pi ND$ rises only from 20.3 m/s to 26.2 m/s — so the pressure rise grows by only about 60 per cent: $$\boxed{\ \Delta p_2=392.5\ \text{Pa}=40.0\ \text{mm H}_2\text{O}\ }$$
  5. Scale the shaft power. Equating power coefficients, $$P_2=P_1\left(\frac{\rho_2}{\rho_1}\right)\left(\frac{N_2}{N_1}\right)^{3} \left(\frac{D_2}{D_1}\right)^{5} =250\times0.9640\times0.13696\times97.656.$$ The fifth power of the diameter ratio is what dominates, and the result is $$\boxed{\ P_2=3.22\ \text{kW}\ }$$ about thirteen times the test power for a machine only 2.5 times larger in diameter.
  6. Confirm the answer set is self-consistent through the efficiency. The statement "efficiency unchanged" is not an extra assumption we may forget — it is a check. Total-to-total efficiency is $\eta=Q\,\Delta p/P$, so for the tested machine $\eta_1=(0.7\times245.17)/250=0.686$ and for the scaled machine $\eta_2=(5.6379\times392.49)/3223.5=0.686$. The two agree to three figures, which they must, because $\phi\psi/\Pi_P$ is itself a dimensionless group; any slip in one of the three exponents above would have shown up here as a mismatch.
QuantityScaling law Value for the 1 m fan at 500 rpm
Air density (state 2)ρ = p/RT1.221 kg/m3
Volume flow rate Q2(N2/N1)(D2/D1)35.64 m3/s
Fan total pressure Δp2(ρ2/ρ1)(N2/N1)2(D2/D1)2392.5 Pa = 40.0 mm H2O
Shaft power P2(ρ2/ρ1)(N2/N1)3(D2/D1)53.22 kW
Efficiency (check)η = QΔp/P0.686, identical for both
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