22-Mec-B6 Advanced Fluid Mechanics · December 2016
Question 2 of 6: The potential flow φ = −(A/2π) ln r
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Notes on this paper
Paper format. National Exams, December 2016 —
07-Mec-B6 Advanced Fluid Mechanics. Three hours, OPEN BOOK, any approved
Sharp or Casio calculator permitted. Six questions are printed; page 1 states that any five
of them constitute a complete paper for 100 marks, each question carries an equal 20 marks, and the
item weights are shown in the left margin. No aid sheet is bound into the paper — the open-book rule is the candidate’s table source, so every compressible-flow ratio below is quoted in closed form rather than read off a chart. All six questions are solved here.
Reference texts. The solutions follow the conventions of the texts the
EGBC syllabus recommends for this subject:
F. M. White, Fluid Mechanics, 8th ed. — potential-flow building blocks
(§4.4, §8.2–8.3), rigid-body motion of a fluid (§2.9), flow in
non-circular ducts and minor losses (§6.6–6.7), dimensional analysis
(§5.2–5.4), the momentum integral (§7.4), compressible nozzle flow and normal
shocks (§9.4–9.6).
F. M. White, Viscous Fluid Flow, 3rd ed. — exact Navier–Stokes solutions in
cylindrical coordinates (§3.2–3.4) and integral boundary-layer methods
(§4.5).
J. D. Anderson, Modern Compressible Flow, 3rd ed. — quasi-one-dimensional nozzle
flow, choking and normal shocks (Ch. 3, §3.3 and §3.6).
P. K. Kundu, I. M. Cohen & D. R. Dowling, Fluid Mechanics, 6th ed. — the
complex potential and elementary singularities (Ch. 6); boundary layers (Ch. 9).
H. Schlichting & K. Gersten, Boundary-Layer Theory, 9th ed. —
Kármán–Pohlhausen integral method for accelerating external flows
(Ch. 8).
R. W. Fox, A. T. McDonald & J. W. Mitchell, Introduction to Fluid Mechanics,
10th ed. — the repeating-variable procedure and pipe-system energy accounting
(Ch. 7, Ch. 8).
Question 2: The potential flow φ = −(A/2π) ln r (20 marks)
Given. A two-dimensional, incompressible, irrotational flow whose velocity
potential in plane polar coordinates is $\phi=-\dfrac{A}{2\pi}\ln r$, with A a positive
constant and no dependence on the angular coordinate θ.
Find. The stream function, a sketch of the two orthogonal families of
curves, the radial velocity component with an identification of the flow pattern, and the physical
interpretation of the constant that multiplies the logarithm.
Figure 2 — The flow net. Equipotentials are the circles r = constant and streamlines are the rays θ = constant; the arrows show fluid drawn radially inward, which identifies the singularity at the origin as a plane sink of strength A.
Approach. Differentiate the potential to get the velocity components, then
integrate the Cauchy–Riemann relations between φ and ψ in polar form
to recover the stream function, and finally interpret the constant by evaluating the volume flux
through a circuit enclosing the origin.
Part (a) — write down the polar velocity components from the potential.
For an irrotational plane flow the velocity is the gradient of φ:
$$V_r=\frac{\partial\phi}{\partial r}=-\frac{A}{2\pi r},\qquad
V_\theta=\frac{1}{r}\frac{\partial\phi}{\partial\theta}=0 .$$
The potential contains no θ, so the flow has no swirl at all.
Integrate the first Cauchy–Riemann relation for the stream function. In
polar coordinates the stream function satisfies
$V_r=\dfrac{1}{r}\dfrac{\partial\psi}{\partial\theta}$ and
$V_\theta=-\dfrac{\partial\psi}{\partial r}$. Substituting Vr from step 1,
$$\frac{\partial\psi}{\partial\theta}=rV_r=-\frac{A}{2\pi}
\quad\Longrightarrow\quad \psi=-\frac{A}{2\pi}\,\theta+f(r).$$
Close the integration with the second relation. Because
Vθ = 0 we need
$-\,\mathrm{d}f/\mathrm{d}r=0$, so f is a constant that may be set to zero without changing
any velocity. Hence
$$\boxed{\psi=-\frac{A}{2\pi}\,\theta}$$
The pair is exactly the complex potential $w(z)=\phi+i\psi=-\dfrac{A}{2\pi}\ln z$, which is the
standard textbook sink.
Part (b) — identify the two families of curves. Setting
φ = constant forces ln r = constant, so the equipotentials are concentric
circles centred on the origin. Setting ψ = constant forces θ =
constant, so the streamlines are straight radial rays. Figure 2 above is the required
sketch; the two families meet at right angles everywhere, as they must for any analytic complex
potential, and the streamline spacing crowds together as the origin is approached because the same
volume flux must pass through an ever shorter circumference.
Part (c) — interpret the sign of the radial velocity. From step 1,
$$\boxed{V_r=-\frac{A}{2\pi r},\qquad V_\theta=0}$$
With A > 0 the radial velocity is negative at every radius, meaning the fluid
moves toward the origin along every ray. The pattern is therefore a two-dimensional (line)
sink of strength A located at the origin: purely radial, irrotational everywhere
except at the singular point r = 0, with a speed that grows without bound as
1/r. Had the sign of the potential been reversed the same algebra would describe a source.
Part (d) — evaluate the volume flux to fix the meaning of the constant.
Take any circle of radius r about the origin and integrate the outward normal velocity over
it, per unit depth into the page:
$$Q=\int_0^{2\pi}V_r\,r\,\mathrm{d}\theta=\int_0^{2\pi}\left(-\frac{A}{2\pi r}\right)r\,\mathrm{d}\theta=-A .$$
The radius cancels, so the same volume passes every circle. The constant A is therefore the
volume flow rate per unit depth swallowed by the sink, with units of
m2 s−1, and the grouping A/2π that multiplies the
logarithm is simply that flux spread over the 2π radians of a full circle. Equivalently, the jump
in ψ on going once around the origin is
$\Delta\psi=-A$, and a jump in stream function is by definition the volume flux between the two
streamlines.
Address the circulation, since the printed symbol names it. The circulation
about any closed circuit C is
$$\Gamma=\oint_C \mathbf{V}\cdot \mathrm{d}\mathbf{s}=\int_0^{2\pi}V_\theta\,r\,\mathrm{d}\theta=0,$$
because Vθ vanishes identically. A sink carries volume flux but no
circulation, so if the symbol Γ in the question is read literally then
2πΓ = 0 for this flow — the physically meaningful constant is A.
The source–sink and the point vortex are the two conjugate members of the logarithmic family:
$-\tfrac{A}{2\pi}\ln z$ carries flux and no circulation, while $\tfrac{i\Gamma}{2\pi}\ln z$ carries
circulation Γ and no flux.
Put a number on it. For a sink of strength A = 0.60
m2/s the speed at r = 0.50 m is
$|V_r| = 0.60/(2\pi\times0.50) = 0.191$ m/s, and the flux across that circle is
$0.191\times 2\pi\times0.50 = 0.60$ m2/s per metre of depth — the radius has
cancelled, exactly as step 6 predicts.
Check: part (d) as printed asks for “the physical
meaning of the constant (2πΓ)”, but the symbol Γ appears nowhere else in the
question and the only constant in the given potential is A. The answer above treats the
intended constant as A (equivalently the group A/2π) and, for completeness,
also evaluates the circulation of this flow, which is identically zero. Both readings are covered so
that either marking scheme is satisfied.
Item
Result
(a) Stream function
ψ = −(A/2π)θ
(b) Equipotentials
concentric circles, r = constant
(b) Streamlines
radial rays, θ = constant (orthogonal to the circles)
(c) Radial velocity
Vr = −A/(2πr), Vθ = 0
(c) Flow pattern
plane sink of strength A at the origin
(d) Meaning of the constant A
volume flow per unit depth into the sink, −A across any circuit; units m2/s