22-Mec-B6 Advanced Fluid Mechanics · Undated paper
Question 4 of 6: Rigid-body rotation of a liquid — Navier–Stokes reduction and the free surface
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Notes on this paper
Paper format. National Exams, May 2019 —
printed code 16-Mec-A6Advanced Fluid Mechanics (the cover page and every running header read 16-Mec-A6, May 2019). Three hours, OPEN BOOK, any approved Sharp or Casio calculator permitted. Six questions are printed; any five of them constitute a complete paper for 100 marks, each question carries an equal 20 marks, and the item weights are printed 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 from 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. — control-volume momentum (§3.4),
potential-flow building blocks (§4.4, §8.2–8.3), dimensional analysis and
modelling (§5.2–5.4), turbulent flat-plate layers (§7.4), isentropic and
normal-shock relations (§9.3–9.5).
J. D. Anderson, Modern Compressible Flow, 3rd ed. — quasi-one-dimensional
nozzle flow and normal shocks (Ch. 3 and Ch. 5).
F. M. White, Viscous Fluid Flow, 3rd ed. — exact solutions of the
Navier–Stokes equations (§3.2).
P. K. Kundu, I. M. Cohen & D. R. Dowling, Fluid Mechanics, 6th ed. —
complex potential and plane potential flows (Ch. 6); boundary layers (Ch. 9).
R. W. Fox, A. T. McDonald & J. W. Mitchell, Introduction to Fluid Mechanics,
10th ed. — momentum analysis of pipe bends (Ch. 4) and similitude (Ch. 7).
SI units throughout. Air and mercury properties are those printed in the question; all pressures
are absolute unless a gauge value is stated explicitly. Water and air properties not printed in the
paper are taken from the standard Canadian-edition property tables at the stated temperatures, and
each such value is named where it is used.
Question 4: Rigid-body rotation of a liquid — Navier–Stokes reduction and the free surface (20 marks)
Given. An incompressible Newtonian liquid of constant density $\rho$ and viscosity
$\mu$ filling a cylindrical container that has been spinning long enough about its vertical axis for
all relative motion to have died out. The velocity field is therefore that of a rigid body,
$$V_r = 0,\qquad V_\theta = \omega r,\qquad V_z = 0$$
with $\omega$ constant, and gravity acts as $\mathbf{g} = -g\,\hat{\mathbf{k}}$. Nothing depends on
$\theta$ or on time.
Find. The reduced $r$- and $z$-momentum equations with a justification for
discarding the viscous terms; the pressure field $p(r,z)$ obtained by integrating them; and a
demonstration that the free surface is the paraboloid $z_s = \omega^{2}r^{2}/2g$.
[Figure not reproduced: Figure 4 (redrawn). Rigid-body rotation. The free surface (blue) and every constant-pressure surface inside the fluid (dashed) are congruent paraboloids of revolution, all with the same curvature $\omega^{2}/2g$. See the official exam paper.]
Approach. Substitute the rigid-body velocity field into the incompressible
Navier–Stokes equations in cylindrical coordinates, show that both the convective and the viscous
terms collapse, integrate the two surviving partial derivatives, and then impose $p = p_{atm}$ on the
free surface.
Reduce the $r$-momentum equation (part a). The steady, axisymmetric
$r$-component of the Navier–Stokes equations in cylindrical coordinates is
$$\rho\left(V_r\frac{\partial V_r}{\partial r} - \frac{V_\theta^{2}}{r} + V_z\frac{\partial V_r}{\partial z}\right)
= -\frac{\partial p}{\partial r} + \mu\left[\frac{\partial}{\partial r}\left(\frac{1}{r}\frac{\partial (rV_r)}{\partial r}\right) + \frac{\partial^{2}V_r}{\partial z^{2}}\right]$$
With $V_r = V_z = 0$ the only surviving inertia term is the centripetal one, $-\rho V_\theta^{2}/r$,
and the entire viscous bracket vanishes because $V_r \equiv 0$. Hence
$$\frac{\partial p}{\partial r} = \rho\,\frac{V_\theta^{2}}{r} = \rho\,\frac{(\omega r)^{2}}{r}
= \rho\,\omega^{2} r$$
Reduce the $z$-momentum equation. With $V_z \equiv 0$ every inertia term and every
viscous term drops, leaving only the pressure gradient and the body force:
$$0 = -\frac{\partial p}{\partial z} - \rho g
\qquad\Longrightarrow\qquad \frac{\partial p}{\partial z} = -\rho g$$
The vertical direction is therefore purely hydrostatic, exactly as in a stationary tank.
Justify discarding the viscous stresses. This is the conceptual heart of
part (a), and it is not the usual “high Reynolds number” argument — the viscous
terms here are identically zero, not merely small. Viscous stress in a Newtonian fluid is
proportional to the rate of deformation, and a rigid-body motion has none: every fluid element
translates and rotates but never strains. Formally, the only candidate shear component in this field is
$$\tau_{r\theta} = \mu\,r\,\frac{\partial}{\partial r}\!\left(\frac{V_\theta}{r}\right)
= \mu\,r\,\frac{\partial}{\partial r}(\omega) = 0$$
because $V_\theta/r = \omega$ is a constant. Likewise the $\theta$-momentum viscous operator gives
$$\frac{\partial}{\partial r}\left[\frac{1}{r}\frac{\partial (rV_\theta)}{\partial r}\right]
= \frac{\partial}{\partial r}\left[\frac{1}{r}\frac{\partial (\omega r^{2})}{\partial r}\right]
= \frac{\partial}{\partial r}\left(2\omega\right) = 0$$
So the fluid behaves inviscidly no matter how viscous it is; viscosity was essential only in the
transient that established the rigid-body state, by diffusing the wall’s rotation into
the interior. The no-slip condition is satisfied automatically once that state is reached, since the
fluid at the wall turns with the wall.
Integrate the radial equation (part b). Integrating
$\partial p/\partial r = \rho\omega^{2}r$ at fixed $z$,
$$p(r,z) = \frac{\rho\,\omega^{2}r^{2}}{2} + f(z)$$
where $f$ is an arbitrary function of $z$ alone — it is a function, not a constant, because the
integration was partial.
Close it with the vertical equation. Differentiating the result of step 4 with
respect to $z$ and matching step 2,
$$\frac{\partial p}{\partial z} = f'(z) = -\rho g \qquad\Longrightarrow\qquad f(z) = -\rho g z + C$$
Writing $C = p_0$, the pressure at the origin $(r,z) = (0,0)$, the complete field is
$$\boxed{p(r,z) = p_0 + \frac{\rho\,\omega^{2}r^{2}}{2} - \rho\,g\,z}$$
valid everywhere in the fluid. It is the ordinary hydrostatic distribution plus a centrifugal term
that raises the pressure quadratically with radius — the mathematical statement of why the liquid
piles up at the rim.
Impose the free-surface condition (part c). The free surface is the locus on which
the pressure equals the atmospheric value. Choosing the origin at the lowest point of the surface, on
the axis, makes $p_0 = p_{atm}$; measuring $p$ as a gauge pressure then sets $p_0 = 0$, and the surface
is the curve $p(r,z_s) = 0$:
$$0 = \frac{\rho\,\omega^{2}r^{2}}{2} - \rho\,g\,z_s$$
Dividing through by $\rho g$ (both non-zero) gives
$$\boxed{z_s = \frac{\omega^{2} r^{2}}{2g}}$$
which is the required result — a paraboloid of revolution. Two structural remarks close the
question. First, every other isobar has exactly the same shape, merely shifted vertically, because
setting $p = $ const in the boxed field of step 5 always gives $z = \omega^{2}r^{2}/2g + $ const.
Second, a paraboloid encloses half the volume of its bounding cylinder, so conservation of liquid
volume fixes the vertical position of the vertex: the axis level drops by exactly the same amount as
the rim level rises, each equal to $\omega^{2}R^{2}/4g$ for a container of radius $R$. For a
150 mm-radius container spinning at 12 rad/s, for example, the rim-to-axis difference is
$\omega^{2}R^{2}/2g = 165\;\text{mm}$, of which 82.6 mm is a rise at the rim and 82.6 mm a
fall on the axis.
Item
Result
(a) $r$-momentum, reduced
$\partial p/\partial r = \rho\,\omega^{2} r$
(a) $z$-momentum, reduced
$\partial p/\partial z = -\rho g$
(a) Why viscous stresses drop
Rigid-body motion has zero rate of strain: $\tau_{r\theta} = \mu r\,\partial(V_\theta/r)/\partial r = 0$ identically
(b) Pressure field
$p(r,z) = p_0 + \rho\omega^{2}r^{2}/2 - \rho g z$
(c) Free surface
$z_s = \omega^{2}r^{2}/2g$ — a paraboloid of revolution
Volume constraint (bonus)
Axis falls and rim rises by $\omega^{2}R^{2}/4g$ each