Question 5 of 6: Question 5 (Part B, Question B2): Potential-Flow Model of a Pool Recirculating System
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Notes on this paper
Paper format. National Exams, May 2013 — 07-Mec-B6
Advanced Fluid Mechanics. Three hours, open book, any non-communicating
calculator permitted. Part A holds three questions of 20 marks each (40 per cent of the
paper) and Part B three questions of 30 marks each (60 per cent); the candidate answers
any two in each part. All six questions are worked here, because the set is a
study resource rather than a three-hour sitting. The paper supplies an aid sheet of compressible-flow,
boundary-layer, Navier–Stokes and potential-flow relations, and the coefficients quoted below
are taken from that sheet so that 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), Ch. 7 (external flow), Ch. 8 (potential flow), Ch. 9 (compressible flow),
Ch. 10 (open-channel flow).
F. M. White, Viscous Fluid Flow, 3rd ed. — Ch. 3 (exact solutions of the
Navier–Stokes equations), Ch. 6 (turbulent wall flow).
J. D. Anderson, Modern Compressible Flow, 3rd ed. — Ch. 3 (normal shock waves),
Ch. 5 (quasi-one-dimensional nozzle flow).
P. K. Kundu, I. M. Cohen and D. R. Dowling, Fluid Mechanics, 6th ed. —
Ch. 6 (irrotational flow), Ch. 9 (laminar flow).
H. Schlichting and K. Gersten, Boundary-Layer Theory, 8th ed. — Ch. 21
(plate drag, mixed laminar/turbulent layers).
R. W. Fox, A. T. McDonald and J. W. Mitchell, Introduction to Fluid Mechanics,
10th ed. — Ch. 7 (similitude), Ch. 11 (open-channel flow).
Question 5 (Part B, Question B2): Potential-Flow Model of a Pool Recirculating System (30 marks)
Find. A stream function that represents the pool, proof that the
floor is a streamline, the sink strength M, and the pressure difference between the two floor
taps.
Figure 5.1 — Potential-flow model of the pool. The supply pipe is a line source at height a; an image source at depth a below the floor makes y = 0 a streamline; the drain is a line sink of strength M sitting on the floor at the origin.
Approach. Build the flow by superposition of elementary
irrotational solutions — a line source for the pipe, its mirror image to make the floor
impermeable, and a line sink at the origin for the drain — then close the mass balance to
size the sink and apply Bernoulli along the floor for the pressure difference.
Part (a) — choose the elementary singularities. With gravity
neglected and the pool very large, the flow away from the pipe and the drain is inviscid and
irrotational, so Laplace's equation governs and solutions may simply be added. The pipe is a line
source of strength $m$ at $(0,a)$, whose stream function is
$\psi = \tfrac{m}{2\pi}\theta$ measured about its own centre. The drain is a line sink of
strength $M$ at the origin. Left alone these two do not satisfy the floor, so a third element is
needed.
Part (a) — enforce the floor with an image. The floor
$y = 0$ must be impermeable, and the method of images supplies exactly that: place an identical
source of strength $m$ at the mirror point $(0,-a)$. The complete stream function in the pool is
then
$$\psi(x,y) = \frac{m}{2\pi}\left[\arctan\!\frac{y-a}{x} + \arctan\!\frac{y+a}{x}\right]
- \frac{M}{2\pi}\arctan\!\frac{y}{x}$$
with the corresponding velocity potential
$\phi = \tfrac{m}{2\pi}\left[\ln r_1 + \ln r_2\right] - \tfrac{M}{2\pi}\ln r_0$, where
$r_1$, $r_2$ and $r_0$ are the distances from the pipe, its image and the drain.
Part (a) — verify that the floor is correctly modelled. The test is
that the normal velocity vanishes on $y = 0$. The real source contributes a vertical velocity
$-\tfrac{m}{2\pi}\tfrac{a}{x^{2}+a^{2}}$ there and the image contributes
$+\tfrac{m}{2\pi}\tfrac{a}{x^{2}+a^{2}}$, which cancel exactly; the sink at the origin drives
purely radial flow along the floor and so contributes no vertical velocity either. Hence
$$v(x,0) = 0 \quad \text{for all } x \neq 0
\;\Longrightarrow\; \boxed{y = 0 \text{ is a streamline}}$$
Evaluating the stream function confirms it: $\psi = 0$ along the whole positive-$x$ floor and
$\psi = -m$ along the negative-$x$ floor, each a constant, and the jump of exactly $m$ between
them is the flow the drain removes — the drain is the singular point at which the two
half-streamlines terminate.
Part (b) — size the sink by mass balance. The pipe discharges its
full strength $m$ into the pool, since it sits inside the region $y>0$. The drain, however, lies
on the boundary: a line sink of strength $M$ placed at the origin draws fluid from all
directions, but only the half of its intake that lies in $y > 0$ is real water. Balancing what
enters against what leaves,
$$m = \tfrac{1}{2}M \;\Longrightarrow\; M = 2m
= \boxed{2\ \text{m}^{3}\text{/s per metre}}$$
The factor of two is easy to lose and is the crux of this part: a drain in the floor must be given
twice the nominal strength of the source it balances.
Part (c) — velocity along the floor. Adding the three horizontal
contributions at a point $(x,0)$ — source, image and sink — gives
$$u(x,0) = \frac{m}{2\pi}\frac{x}{x^{2}+a^{2}} + \frac{m}{2\pi}\frac{x}{x^{2}+a^{2}}
- \frac{2m}{2\pi}\frac{1}{x} = -\,\frac{m\,a^{2}}{\pi\,x\,(x^{2}+a^{2})}$$
The result is negative for $x>0$, confirming that the floor flow runs back toward the drain, and
it decays like $x^{-3}$ far away because the source and its image form a doublet-like pair when
seen from a distance.
Part (c) — evaluate at the two taps. Substituting $m = 1$ and
$a = 3$ m,
$$\begin{aligned}
u_b &= -\frac{(1)(9)}{\pi(1)(1+9)} = -0.2865\ \text{m/s} \\
u_c &= -\frac{(1)(9)}{\pi(2)(4+9)} = -0.1102\ \text{m/s}
\end{aligned}$$
so the water is moving roughly two and a half times faster at the inner tap than at the outer one.
Part (c) — apply Bernoulli along the floor. The floor is a
streamline of a steady irrotational flow with gravity neglected, so
$p + \tfrac12\rho u^{2}$ is the same at both taps:
$$p_b - p_c = \tfrac{1}{2}\rho\left(u_c^{2} - u_b^{2}\right)
= \tfrac{1}{2}(1000)\left[(-0.1102)^{2} - (-0.2865)^{2}\right]
= \boxed{-35.0\ \text{Pa}}$$
The negative sign says the inner tap reads the lower pressure, by
35.0 Pa, which is what one expects where the flow accelerates into the
drain. A gauge connected between the two taps would read about
35 Pa, and because the reading scales as the square of the source
strength it is a sensitive monitor of the recirculation rate.
Final Results.
Quantity
Symbol
Value
Stream function (a)
ψ
(m/2π)[θ1 + θ2] − (M/2π)θ0 (source at y = a, image at y = −a, sink at the origin)
Floor check (a)
v(x,0)
0 for all x ≠ 0; ψ constant on each half of the floor