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2D-flow in a tube: Continuity and Navier-Stokes |
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August 9, 2017, 12:55 |
2D-flow in a tube: Continuity and Navier-Stokes
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#1 |
New Member
Join Date: Aug 2017
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Hi people,
I want to do some basic stuff with Python 2.7 an the finite differences method. Now I have the following case: - 2D-flow in a tube, steady state, not compressible - at the inlet there ist a constant velocity profile so () - the flow is developing into a convex profile I want to find out the length "L" of the tube, where the velocity profile isn't developing any more. The basic equation for continuity and Navier-Stokes are: An assumption is, that I say the velocity "v" is everywhere zero. So every term with "v" in the Navier-Stokes and Continuity equation is zero and I have to solve only the u-Momentum (as shown). In addition to this I say that is also zero. After this assumptions I have these equations left (Continuity and navier-stokes): If I look to my continuity equation and insert it into the navier-stokes, there is: So in my eyes it doesn't make sense ? It means: The velocity profile is not dependent on the fluid. So it doesn't matter, if there is water or air ? I don't think so.(?) I tried the case without inserting and I solved the equation in Python. It works and there are meaningful results. But I don't understand. Actually I have to insert the continuity into the Navier-stokes, isn't it ? |
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August 10, 2017, 15:31 |
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#2 |
Senior Member
Join Date: Jul 2009
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For steady continuity a non-zero gradient du/dx in the flow will have to be accompanied by a non-zero dv/dy, hence v cannot be zero everywhere. I think you have made too many assumptions and the apparent conflict in your results is indicative of this. Once you reach fully developed flow, du/dx is zero and the pressure gradient is balanced by the viscous stress. Then v is zero. But in the development region you cannot make this assumption.
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August 10, 2017, 16:03 |
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#3 |
Senior Member
Filippo Maria Denaro
Join Date: Jul 2010
Posts: 6,773
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What you are trying to do is the study of the developing boundary layer along a flat plate (top and bottom walls), so you have to use the Prandtl equations.
Just consider that the flow evolves until the thickness of the BL is equal to H/2 (H the distance between the two walls). You can use the law delta(x) to compute this lenght that depends on the viscosity of the fluid (or Re number). A FD solver can be used to check the theory. |
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August 10, 2017, 16:47 |
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#4 |
Senior Member
Lucky
Join Date: Apr 2011
Location: Orlando, FL USA
Posts: 5,675
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You've made way too many assumptions. Your solution is u=constant everywhere, which doesn't even make sense.
du/dy=0 is only at the inlet, not everywhere. This should be obvious in a pipe flow because u=something at the inlet but u=0 on walls because of the no-slip condition. From where do you get dp/dx=0 ? Even for a flat plate dp/dx is not zero and for a pipe it must eventually be a non-zero constant when the flow in the pipe is fully developed. From where do you get v = 0? This is the advection-diffusion equation for a parallel flow (flows very small gradients in the y direction). If you solve this equation, you will indeed get a result that looks like a flow because it is an advection equation. But it has limitations. For learning finite differences this is actually a really good equation to try and solve because it contains non-linear advection on top of diffusion. Usually diffusion problems are 1st problem introduced. |
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August 11, 2017, 09:42 |
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#5 |
Senior Member
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I think you should not make any assumption since the velocity is developing.
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