Question 2 of 6: Discharge pipe above a tank bed with a drain
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Notes on this paper
Paper format. National Exams, May 2016 —
07-Mec-B6 Advanced Fluid Mechanics. Three hours, OPEN BOOK, any
approved Sharp or Casio calculator permitted. Six questions are printed; any five
of them constitute a complete paper, each carries an equal 20 marks, and the item weights
are shown in the left margin. No aid sheet is bound into this 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. 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), laminar boundary layers and the momentum integral
(§7.2–7.4), dimensional analysis (§5.2–5.4), compressible duct
flow (§9.5–9.7).
F. M. White, Viscous Fluid Flow, 3rd ed. — exact solutions of the
Navier–Stokes equations 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, normal shocks and Fanno flow (Ch. 3, Ch. 5).
P. K. Kundu, I. M. Cohen & D. R. Dowling, Fluid Mechanics, 6th ed. —
complex potential, images and the Blasius/Lagally force theorems (Ch. 6); boundary
layers (Ch. 9).
B. R. Munson et al., Fundamentals of Fluid Mechanics, 8th ed. —
Buckingham Pi method and the repeating-variable procedure (Ch. 7).
Question 2: Discharge pipe above a tank bed with a drain (20 marks)
Given. A two-dimensional line source of strength m
representing the discharge pipe, sitting a height b above a flat, impermeable tank
bed; a line sink of strength −2m representing the drain, located on
the bed directly beneath the pipe; fluid density ρ; quiescent fluid far away; free-surface
effects neglected. Coordinates are taken from the figure: x along the bed,
y vertically upward, origin at the drain, so the pipe sits at (0, b).
Find. A stream function for the flow, a demonstration that it really does
reproduce the flat bed, the velocity distribution along that bed, and the resultant force per
unit length that the flow exerts on the discharge pipe.
[Figure not reproduced: Figure 2 (redrawn) with the image system added. Mirroring the source in the bed makes y = 0 a streamline; the drain sits on the plane of symmetry, so its printed strength −2 m already includes its own image and exactly absorbs the 2 m the source pair emits. See the official exam paper.]
Approach. Build the flow from three elementary singularities
— the real source, its image in the bed, and the drain — then verify the wall by
showing the normal velocity vanishes, differentiate for the bed velocity, and evaluate the
force with the Blasius/Lagally theorem, whose one non-obvious ingredient is that the
singularity does not act on itself.
Throughout, a line source of strength m is taken in the standard convention
$$\psi=m\theta,\qquad \phi=m\ln r,\qquad u_r=\frac{m}{r},$$
so the volume discharged per unit length of pipe is Q = 2πm. (Papers
that define the strength as the discharge itself simply replace m by
Q/2π everywhere below; every formula that follows is homogeneous of degree two in
m, so nothing else changes.)
Part (a) — place the image and write the stream function. A plane
wall is reproduced by reflecting each singularity in it with the same sign for a
source. Mirroring the pipe at (0, b) puts an image source of strength
m at (0, −b). The drain already lies on the wall, so its image
coincides with itself — which is exactly why the paper prints its strength as
−2m. Superposing the three,
$$\boxed{\;\psi(x,y)=m\arctan\!\frac{y-b}{x}+m\arctan\!\frac{y+b}{x}-2m\arctan\!\frac{y}{x}\;}$$
with each arctangent understood as the two-argument form measured from the positive
x axis.
Check the mass budget before going further. In the full-plane model the
source pair emits 2π(2m) and the drain absorbs 2π(2m): the system is
closed, which is the physical statement that the drain removes exactly what the pipe
discharges. Had the drain been given strength −m, half the discharge would
have had to escape to infinity and the far-field “quiescent” assumption in the
question would be violated.
Part (b) — verify the bed. The bed is correctly simulated if the
normal velocity vanishes on it. Differentiating the superposition, the vertical
component at a general point is
$$v=\frac{m(y-b)}{x^{2}+(y-b)^{2}}+\frac{m(y+b)}{x^{2}+(y+b)^{2}}-\frac{2my}{x^{2}+y^{2}},$$
and setting y = 0 the first two terms cancel identically while the third vanishes:
$$v(x,0)=\frac{-mb}{x^{2}+b^{2}}+\frac{mb}{x^{2}+b^{2}}-0=0\quad\text{for all }x\neq 0 .$$
So y = 0 is a streamline and the bed is exactly reproduced.
A warning about testing the wall with ψ instead of v.
Evaluating the stream function on the bed gives ψ = 0 for x > 0 but
ψ = −2πm for x < 0. That jump is not a failure: it equals
the volume flux the drain removes, and any streamline function must be multivalued across a
sink placed on the boundary. The physically meaningful test is the vanishing normal
velocity in Step 3, and it is the test to present.
Part (c) — the velocity along the bed. The horizontal component is
$$u=\frac{mx}{x^{2}+(y-b)^{2}}+\frac{mx}{x^{2}+(y+b)^{2}}-\frac{2mx}{x^{2}+y^{2}},$$
which on y = 0 collapses neatly:
$$u(x,0)=\frac{2mx}{x^{2}+b^{2}}-\frac{2m}{x}=2m\,\frac{x^{2}-(x^{2}+b^{2})}{x\,(x^{2}+b^{2})}$$
$$\boxed{\;u(x,0)=-\frac{2mb^{2}}{x\,(x^{2}+b^{2})},\qquad v(x,0)=0\;}$$
The sign is the physically satisfying part: u is negative for x > 0 and
positive for x < 0, so the bed flow converges on the drain from both directions,
as it must when the drain swallows the entire discharge. The speed decays like
2mb2/x3 far away and grows without bound at the drain
itself, where the point-sink idealisation loses meaning within a radius of order the real
drain opening.
Part (d) — set up the force calculation. Work with the complex
potential of the whole system,
$$w(z)=m\ln(z-ib)+m\ln(z+ib)-2m\ln z,\qquad \frac{dw}{dz}=u-iv .$$
The Blasius theorem applied to a small contour around the pipe, combined with the fact that
a singularity exerts no force on itself, gives the Lagally result
$$X-iY=-2\pi\rho\,m\,W_{0},$$
where W0 is the complex velocity of everything except the pipe
itself, evaluated at the pipe’s own position.
Evaluate the induced velocity at the pipe. At
z0 = ib the image and the drain contribute
$$W_{0}=\frac{m}{ib+ib}+\frac{-2m}{ib}=-\frac{im}{2b}+\frac{2im}{b}=\frac{3im}{2b}.$$
The image alone would push the pipe upward at m/2b; the drain, being twice
as strong and only half as far in this sense, reverses and triples the result.
Collect the force. Substituting,
$$X-iY=-2\pi\rho m\left(\frac{3im}{2b}\right)=-\frac{3i\pi\rho m^{2}}{b},$$
so that
$$\boxed{\;X=0,\qquad Y=+\frac{3\pi\rho m^{2}}{b}\ \ \text{per unit length (directed away from the bed)}\;}$$
The horizontal force vanishes because the image and the drain are both on the vertical axis
through the pipe, leaving nothing to break the left–right symmetry.
Sanity-check against the classical wall result. Switch the drain off and
the same formula returns
Y = −πρm2/b — the textbook result
that a source is attracted to a nearby wall, which can be confirmed independently by
integrating the bed pressure. Turning the drain on flips the sign and multiplies the
magnitude by three: the pipe is pushed away from the bed. That reversal is the engineering
message for the supervisor — opening the drain does not merely change the load on the
pipe supports, it changes its direction.
Put numbers on it. For a discharge of
Q = 0.40 m3/s per metre of pipe (so m = Q/2π =
0.0637 m2/s), a standoff b = 1.5 m and ρ = 998 kg/m3,
$$Y=\frac{3\pi(998)(0.0637)^{2}}{1.5}=25.4\ \text{N/m (upward)},$$
and the bed speed one metre from the drain is
2(0.0637)(1.5)2/[1.0(1.0 + 2.25)] = 0.088 m/s — slow enough that scour is not
a concern, while the 25 N per metre of uplift is a real design load on a long pipe run.
Part
Quantity
Result
(a)
Stream function
ψ = m atan2(y−b, x) + m atan2(y+b, x) − 2m atan2(y, x)
(b)
Bed condition
v(x, 0) = 0 for all x ≠ 0 — the bed is a streamline
(c)
Bed velocity
u(x, 0) = −2mb2/[x(x2 + b2)], v = 0
(d)
Horizontal force on the pipe
X = 0
(d)
Vertical force on the pipe
Y = +3πρm2/b, directed away from the bed
(d)
Illustrative value (Q = 0.40 m3/s·m, b = 1.5 m)
25.4 N/m uplift
analytically, and by numerically evaluating the Blasius contour integral
(iρ/2)∮(dw/dz)2dz on a small circle around the
pipe. Both agree, and the drain-off limit reproduces the classical
−πρm2/b wall attraction.