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.
F. M. White, Fluid Mechanics, 8th ed. — Ch. 5 (dimensional analysis and
similitude, turbomachine coefficients), Ch. 8 (potential flow and the method of images),
Ch. 9 (compressible duct flow, normal shocks, Fanno flow), Ch. 11 (turbomachinery).
F. M. White, Viscous Fluid Flow, 3rd ed. — Ch. 3 (exact solutions of the
Navier–Stokes equations: film flows, rotating containers).
J. D. Anderson, Modern Compressible Flow, 3rd ed. — Ch. 3 (normal shock
waves), Ch. 5 (quasi-one-dimensional nozzle flow, supersonic wind tunnels).
R. W. Fox, P. J. Pritchard and A. T. McDonald, Introduction to Fluid Mechanics,
10th ed. — Ch. 7 (similitude), Ch. 10 (fluid machinery), Ch. 12–13
(compressible flow).
P. K. Kundu, I. M. Cohen and D. R. Dowling, Fluid Mechanics, 6th ed. —
Ch. 6 (ideal flow, images), Ch. 9 (laminar flow).
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)
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.
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.
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.
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.
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:
$$\boxed{\ Q_2=5.64\ \text{m}^3/\text{s}\ }$$
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:
$$\boxed{\ \Delta p_2=392.5\ \text{Pa}=40.0\ \text{mm H}_2\text{O}\ }$$
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.
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.