Justifying steps in the Navier-Stokes calculation for simple circular pipe flow.

Also if we have a pipe, u_r = 0 and we can have no \theta dependence in u_z. I think this answers all the questions.In summary, the conversation discusses a problem in which a circular pipe with constant pressure gradient is analyzed using the Navier-Stokes equations. It is assumed that the radial and angular components of velocity are zero, leading to the conclusion that the z-component of velocity is also independent of z and \theta. This is justified by considering the pressure gradient as the only external force and applying Newton's second law. Additionally, the equation for incompressible fluids is augmented to account for the pipe geometry, further supporting the assumption of no z or \theta dependence in the velocity components.
  • #1
Peeter
305
3

Homework Statement



In [1], problem 2.3 (ii), we are asked to show that for a pipe with circular cross section [itex]r = a[/itex] and constant pressure gradient [itex]P = -dp/dz[/itex] one has

[tex]u_z = \frac{P}{4 \mu}\left( a^2 - r^2 \right)[/tex]
[tex]u_r = 0[/tex]
[tex]u_\theta = 0[/tex]

References:

[1] D.J. Acheson. <em>Elementary fluid dynamics</em>. Oxford University Press, USA, 1990.

Homework Equations



If one does assume that [itex]u_r = u_\theta = 0[/itex], then the Navier-stokes equations for an incompressible steady state flow takes the form

[tex]\begin{align}u_z \frac{\partial {u_z}}{\partial {z}} = \frac{P}{\rho} + \nu \left(\frac{1}{{r}} \frac{\partial {}}{\partial {r}}\left(r \frac{\partial {u_z}}{\partial {r}} \right) + \frac{\partial^2 {{u_z}}}{\partial {{\theta}}^2} + \frac{\partial^2 {{u_z}}}{\partial {{z}}^2}\right)\end{align} [/tex]
[tex]\begin{align}0 = \frac{\partial {p}}{\partial {r}}\end{align} [/tex]
[tex]\begin{align}0 = \frac{\partial {p}}{\partial {\theta}}\end{align} [/tex]

The Attempt at a Solution



I can actually solve this problem completely, but have some trouble justifying some of the steps.

a) One of them is the assumption that [itex]u_r = u_\theta = 0[/itex], which I use as a starting point to express NS above. This intuitively makes sense, but are there other physical principles (other than intuition) that lead to this conclusion?

b) In NS above we can kill of the [itex]\partial_{\theta\theta}[/itex] portion of the Laplacian, again by intuition. However, it's not too hard to imagine that you could have a flow where one could have an angular dependence in the flow (ie. imagine a really big pipe where fluid is being injected harder at the base of the pipe than at the top). Something like that would probably have a different pressure dependence. It isn't clear to me what sort of mathematical argument that one could use to show that for this constant pressure gradient scenerio one must have no [itex]\theta[/itex] dependence in the velocity.

c) Finally, once we make assumption (b) so that [itex]\partial_\theta u_z = 0[/itex], NS takes the form (with [itex]w = u_z[/itex])

[tex]\begin{align}w \frac{\partial {w}}{\partial {z}} = \frac{P}{\rho} + \nu \left(\frac{1}{{r}} \frac{\partial {}}{\partial {r}}\left(r \frac{\partial {w}}{\partial {r}} \right) + \frac{\partial^2 {{w}}}{\partial {{z}}^2}\right).\end{align} [/tex]

Attempting separation of variables with [itex]w = Z(z) R(r)[/itex], this appears to be inseparable due to the non-linearity of the [itex](\mathbf{u} \cdot \boldsymbol{\nabla}) \mathbf{u}[/itex] term on the LHS. The fact that this is inseparable doesn't seem like it's a good justificaion for requiring that [itex]w = w(r)[/itex] only and not [itex]w = w(r,z)[/itex]. I could imagine that it is still possible to find solutions of the form [itex]w = w(r,z)[/itex]. Is there some other argument that can be made to show that there is no [itex]z[/itex] dependence in this remaining component of the fluid's velocity?
 
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  • #2
I think all of your questions basically have the same answer. Just think of NS as a statement of Newton's second law and it should become obvious.
[tex]\mathbf{F}=m\mathbf{a}[/tex]
becomes
[tex]-\nabla p=\rho\frac{D\boldsymbol{u}}{Dt}[/tex] where the capital D's denote the advective derivative.

(I've written it with no externally applied forces because your question seems to imply that's the case. I don't think the question would make any sense without that assumption.)

Therefore, you should be able to see very clearly that since the pressure gradient (force) only has a z component, there shouldn't be any change in the flow (accelleration) in the radial or angular directions. The pressure field is a constant so the flow is steady--i.e., you don't have to worry about residual currents or changes in the flow as if the question were "at t=0 the pressure field is turned on" or anything like that.

Let me know if this makes sense to you.
 
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  • #3
I think that answers why we'd have no [itex]u_r[/itex], and [itex]u_\theta[/itex] terms, but we have one more (the Laplacian) term in this version of F=ma:

Jolb said:
[tex]\rho \nabla^2 \boldsymbol{u} -\nabla p=\rho\frac{D\boldsymbol{u}}{Dt}[/tex]

with that term it still seems to me that we can have functional dependence on z and [itex]\theta[/itex], even without components directed in the radial or angular directions.

Yes, in this problem, no external forces are being considered.
 
  • #4
Okay, I see why there's no z-dependence in u_z. The statement of the problem should have included one more equation. This was Navier-Stokes for incompressible fluids, so must be augmented by

[tex]\nabla \cdot \mathbf{u} = \frac{1}{r}\partial_r( r u_r) + \frac{1}{r} \partial_\theta u_\theta + \partial_z u_z = 0[/tex]

so if [itex]u_r = u_\theta = 0[/itex], we can have no z dependence in u_z.
 
  • #5


a) The assumption that u_r = u_\theta = 0 can be justified by the fact that the flow in a circular pipe is axially symmetric, meaning that it has the same properties in all directions around the axis of the pipe. This symmetry implies that the velocity components in the radial and tangential directions must be zero, as any non-zero values would break the symmetry. This is a common assumption in many fluid dynamics problems, as it simplifies the equations and allows for easier analysis and solution.

b) The assumption of no angular dependence in the flow (i.e. \partial_\theta u_z = 0) can be justified by the fact that the pressure gradient in the pipe is constant in the z direction. This means that the pressure is the same at all points on a given horizontal plane, regardless of their angular position. If there were an angular dependence in the flow, this would imply a variation in pressure around the pipe, which would contradict the constant pressure gradient assumption. Therefore, it can be concluded that for this specific scenario, the flow must be independent of \theta.

c) The non-linearity of the term on the left-hand side of the Navier-Stokes equation does not necessarily mean that the flow cannot be separable in the form of w = Z(z) R(r). It simply means that the resulting equations will be non-linear, which may make them more difficult to solve. However, even if the equations cannot be solved analytically, numerical methods can still be used to obtain solutions. Additionally, the fact that the equations are non-linear does not affect the justification for the assumption of no z dependence in w. This assumption is based on the previous arguments in parts a) and b) and is independent of the linearity of the equations.
 

1. What is the Navier-Stokes equation and how is it used in simple circular pipe flow calculations?

The Navier-Stokes equation is a fundamental equation that describes the motion of fluids. It takes into account the effects of viscosity, pressure, and velocity on the flow of a fluid. In simple circular pipe flow calculations, this equation is used to calculate the velocity profile, pressure drop, and other flow parameters.

2. How do you justify the steps in the Navier-Stokes calculation for simple circular pipe flow?

The steps in the Navier-Stokes calculation for simple circular pipe flow are justified by using mathematical and physical principles. These include the conservation of mass, momentum, and energy, as well as assumptions such as the fluid being incompressible and the flow being steady and laminar.

3. What are the simplifications made in the Navier-Stokes equation for simple circular pipe flow?

In order to make the Navier-Stokes equation more applicable to simple circular pipe flow, several simplifications are made. These include assuming the fluid to be incompressible, neglecting the effects of turbulence and external forces, and assuming the flow to be steady and laminar.

4. How are boundary conditions applied in the Navier-Stokes calculation for simple circular pipe flow?

Boundary conditions are applied in the Navier-Stokes calculation for simple circular pipe flow to account for the effects of the pipe walls on the flow. These include the no-slip condition, which states that the fluid velocity at the pipe wall is zero, and the continuity condition, which ensures that the fluid flow is continuous at the boundaries.

5. What are the limitations of using the Navier-Stokes equation for simple circular pipe flow calculations?

The Navier-Stokes equation has some limitations when applied to simple circular pipe flow calculations. It assumes certain simplifications and idealizations, which may not accurately reflect real-world conditions. It also becomes more complex and difficult to solve as the flow becomes more turbulent.

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