Fluid Mechanics

Viscous pipe flows

Lecturer: Jakob Hærvig

Slides by Jakob Hærvig (AAU Energy) and Jacob Andersen (AAU Build)

Types of pipe flows

Various pipe flow types exist, each with distinct physics

  • Single phase pipe flows
    • Completely filled with liquid (or gas)
    • Pressure difference ($p_2 - p_1$) drives flow
  • Open channel pipe flow
    • Partially filled with liquid
    • Gravity drives flow
  • Multiphase pipe flow
    • Either partially or full of liquid (or gas)
    • Gravity drives flow
    • Complex physics (bubbles, particles, droplets etc)

Much research focuses on complex multiphase flows (including own PhD)

Numerical simulations provide details on the process, which can be difficult to capture experimentally.

  • Turbulent pipe flow
  • Solid particles with $d_p = 10$ μm
  • Particle agglomeration (sticking) occurs due to van der Waals and electrostatic forces

Video: Agglomeration of particles in a turbulent pipe flow

Why look at viscous pipe flows ?

Laminar and turbulent flows

Characterised by different flow regimes:

  • Turbulent flow: chaotic and irregular (mixing occurs)
  • Transitional flow: between laminar and turbulent
  • Laminar flow: smooth and orderly (no mixing)

Flow regime depends on Reynolds number ($\text{Re}_D=U\rho D/\mu$)

  • $\text{Re}_D > 4000$: Turbulent
  • $2300 < \text{Re}_D < 4000$: Transitional
  • $\text{Re}_D < 2300$ : Laminar

Entrance regions and fully-developed flows

Region close to inlets

  • (1): Inviscid (enters with near uniform velocity aka plug flow)
  • (2): Reaches fully-developed (boundary layer reached centre)
  • (3): Remains fully developed and nothing changes
  • (4): Skewed and starts to develop again
  • (5): Reaches fully-developed again
  • (6): Remains fully-developed and nothing changes

Entrance length $l_e$ depends on Reynolds number:

  • Laminar: \( l_e/D \approx 0.06 \text{Re}_D \)
  • Turbulent: \( l_e/D \approx 4.4 \text{Re}_D^{1/6} \)

Pressure profile in pipe flows

Pressure varies in fully-developed laminar flow linearly along the pipe

  • $\partial p/\partial x= -\Delta p/p < 0$

Pressure drop in pipe flows is balanced by:

  • Pressure drop due to friction (viscous effects)
  • Pressure drop due to acceleration/deceleration of flow (inertia effects)
  • Hydrostatic pressure variation due to elevation changes

Recall from analytical solutions earlier:

    \(Q = \dfrac{\pi R^4}{8\mu} \left(-\dfrac{\partial p}{\partial z}\right)\) \(= \dfrac{\pi D^4}{128\mu} \left(-\dfrac{\partial p}{\partial z}\right)\) \(= \dfrac{\pi D^4 \Delta p}{128\mu l}\)

    • Valid for laminar, steady, horisontal, fully-developed flow

For non-horisontal pipes:

    \( Q =\dfrac{\pi D^4(\Delta p - \rho g l \text{sin}\theta)}{128\mu l}\)

Exercise: Laminar Pipe Flow

An oil with a viscosity of $\mu = 0.1 \, \text{Pa} \cdot \text{s}$ and density $\rho = 900 \, \text{kg/m}^3$ flows in a pipe of diameter $D = 0.020 \, \text{m}$.

  • (a) What pressure drop, $p_1-p_2$, is needed to produce a flowrate of $Q=2.0 \times 10^{-5} \, \text{m}^3/\text{s}$ if the pipe is horizontal with $x_1 = 0$ and $x_2 = 10 \, \text{m}$?
  • (b) How steep a hill, $\theta$, must the pipe be on to if the oil is to flow through the pipe at the same rate as in part (a), but with $p_1=p_2$?
  • (c) For the conditions of part (b), if $p_1=200$ kPa, what is the pressure at section $x_3=5$ m, where $x$ is measured along the pipe?

Transition from laminar to turbulent flow

Happens gradually between $Re \approx 2100$ and $Re \approx 4000$

  • Small bursts of turbulence start at $\text{Re} \approx 2100$
  • Bursts grow in size and frequency with increasing $\text{Re}$
  • Increased mixing and momentum transfer occurs
  • Higher heat transfer rates and pressure drop

Velocity field $\textbf{\textit{V}}$ changes from being 1-D to 3-D

  • Laminar: $\textbf{\textit{V}}=v_x\cdot \hat{\textbf{i}}$
  • Turbulent: $\textbf{\textit{V}}=v_x\cdot \hat{\textbf{i}} + v_y\cdot \hat{\textbf{j}} + v_z\cdot \hat{\textbf{k}}$

Decomposing a turbulent flow

Consider a turbulent flow with instantaneous velocity $u(t)$

  • Time-averaged velocity component $\overline{u}$
  • $$\overline{u}(x,y,z) = \dfrac{1}{T} \int_{t_0}^{T+t_0} u(x,y,z,t) \, \text{d}t$$

    • $T$ is the averaging time period (should be long enough to capture the relevant flow structures)

  • Instantaneous velocity can then be decomposed as:
  • $$u(x,y,z,t) = \overline{u}(x,y,z) + u'(x,y,z,t)$$

  • Fluctuating velocity component $u'$
  • $$u'(x,y,z,t) = u(x,y,z,t) - \overline{u}(x,y,z)$$

Describing turbulence

Relevant to quantify strength of fluctuations

  • Clearly, time-averaging fluctuations $\overline{u'}$ does not make sense
  • $$\overline{u'}(x,y,z) = \dfrac{1}{T} \int_{t_0}^{T+t_0} u'(x,y,z,t) \, \text{d}t = 0$$

  • What if we take square fluctuations and then time-average?
  • $$\overline{(u')^2}(x,y,z) = \dfrac{1}{T} \int_{t_0}^{T+t_0} u'(x,y,z,t)^2 \, \text{d}t > 0$$

  • To get "back" to same order of magnitude, we now take the square root of fluctuations
  • $$u_\text{rms}(x,y,z) = \sqrt{\overline{(u')^2}(x,y,z)}$$

  • This is called the root-mean-square (RMS) of the fluctuations
  • Often normalised by the time-averaged velocity to get a relative measure, aka turbulence intensity
  • $$I(x,y,z) = \dfrac{u_\text{rms}(x,y,z)}{\overline{u}(x,y,z)}$$