Compressible flow or incompressible flow equation?

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Discussion Overview

The discussion revolves around determining whether a flow problem involving nitrogen gas is compressible or incompressible. Participants explore the implications of flow conditions, such as pressure, temperature, and velocity, on the classification of the flow. The context includes the application of the Navier-Stokes equations in a two-dimensional scenario, with considerations of steady-state conditions and the effects of compressibility.

Discussion Character

  • Debate/contested
  • Technical explanation
  • Mathematical reasoning

Main Points Raised

  • Some participants suggest that since nitrogen is a gas, the flow is compressible, but the effects of compressibility might be negligible depending on local Mach numbers.
  • It is proposed that if the highest local Mach number is below 0.1, the flow can be treated as incompressible, while a Mach number above 0.3 necessitates the use of compressible equations.
  • Participants discuss the importance of pressure variations and local Mach numbers in determining the flow type, indicating that small pressure variations relative to static pressure may allow for incompressible treatment.
  • One participant describes a scenario where a high-speed projectile impacts a closed horizontal pipe, affecting flow characteristics and temperature, and questions the appropriate equations to use for velocity calculations.
  • There is a request for assistance in converting equations into a non-dimensional form, highlighting uncertainty in the conditions of the problem.
  • Participants express interest in reviewing an illustration of the problem to better understand the flow dynamics and provide assistance.
  • One participant notes that the particle's speed of 6.5 km/s indicates hypersonic flow, reinforcing the necessity of considering compressibility.
  • There is a question about the appropriateness of illustrating the flow in a half-pipe configuration, indicating concerns about symmetry in the problem setup.

Areas of Agreement / Disagreement

Participants generally agree that the flow is compressible due to the nature of the gas and the high speeds involved, but there is no consensus on the extent to which compressibility effects can be neglected. Multiple competing views on the treatment of the flow remain unresolved.

Contextual Notes

Participants mention the need to compute local Mach numbers and assess pressure variations, indicating that assumptions about flow conditions are critical to the analysis. The discussion reflects uncertainty regarding the correct equations and configurations to use in the context of the problem.

Who May Find This Useful

This discussion may be useful for individuals studying fluid dynamics, particularly those interested in compressible flow analysis, the application of the Navier-Stokes equations, and the implications of high-speed gas flows.

ulfaazmi
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Hello everyone..
I am using 2-dimension Navier Stokes equation, but I confused that my problem is compressible or incompressible flow form, because if I have initial pressure and temperature and velocity for x-axis only in one grid that they are so very high but the others grid are zero. Can I consider the equation is compressible flow??Thank you
 
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Is it a liquid or a gas?
 
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Chestermiller said:
Is it a liquid or a gas?
It is Nitrogen gas.
 
ulfaazmi said:
It is Nitrogen gas.
Then the flow is compressible. Can you provide more details on your difficulty?
 
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Chestermiller said:
Then the flow is compressible.
But the effects of compressibility might be negligible. You should compute the highest local Mach number $$Ma=U/c$$ in your flow. If it is smaller than say 0.1, the effects of compressibility can be ignored and you can use the incompressible Navier Stokes equations. If it is higher than 0.3, then you should definitely use the compressible form.
 
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Chestermiller said:
Then the flow is compressible. Can you provide more details on your difficulty?

Not necessarily. Gas flows can be simplified as incompressible depending on the details - you should look at pressure variation thoughout your flowfield, as well as local mach numbers. If your pressure variations are small relative to the overall static pressure and the local mach number never exceeds 0.3 or so, you can reasonably treat the problem as incompressible.
 
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bigfooted said:
But the effects of compressibility might be negligible. You should compute the highest local Mach number $$Ma=U/c$$ in your flow. If it is smaller than say 0.1, the effects of compressibility can be ignored and you can use the incompressible Navier Stokes equations. If it is higher than 0.3, then you should definitely use the compressible form.

Thank you for your help, actually the driving force of flow is caused by pressure. So, initially the flow is in a steady state in a closed horizontal pipe until pressure is introduced into that flow caused by a high speed projectile hits the wall of pipe. It also affecting temperature becomes higher at the area exactly in the center of the left side of pipe. Can I guess the velocity can be obtained from the equation :
P = ρ/U ?
 
cjl said:
Not necessarily. Gas flows can be simplified as incompressible depending on the details - you should look at pressure variation thoughout your flowfield, as well as local mach numbers. If your pressure variations are small relative to the overall static pressure and the local mach number never exceeds 0.3 or so, you can reasonably treat the problem as incompressible.
Thank you for your help
Chestermiller said:
Then the flow is compressible. Can you provide more details on your difficulty?
Thank you for your help, actually I have problem to get the correct equation of my study. I am difficult to converting the equation into the non dimensional system because the condition is not clear yet. If it doesn't bother you, would you like to check my equation, I will send it in a picture because it is difficult to write here, also include with the illustration of my problem??
 
ulfaazmi said:
Thank you for your help

Thank you for your help, actually I have problem to get the correct equation of my study. I am difficult to converting the equation into the non dimensional system because the condition is not clear yet. If it doesn't bother you, would you like to check my equation, I will send it in a picture because it is difficult to write here, also include with the illustration of my problem??
Sure. Let's see what you got. Just upload it.
 
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  • #10
An illustration of your problem would be very helpful for us to determine the best approach to take.
 
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  • #11
1CTWibwiW33ngNlEEWQLOIKGgMj5I9-sv


I attached my picture file in this link (https://drive.google.com/drive/u/0/folders/1CTWibwiW33ngNlEEWQLOIKGgMj5I9-sv), I am really pleasure if you would like to help me.

Thank you very much.
 
  • #12
That link doesn't work - it says access denied. You could try uploading to a site like imgur or something, or adding an attachment here...
 
  • #13
cjl said:
That link doesn't work - it says access denied. You could try uploading to a site like imgur or something, or adding an attachment here...
I am so sorry about that. Actually, I did not find any tool to send an attachment directly from here. So, as you mentioned like "imgur", I tried to upload my images there, and this is the link "https://imgur.com/a/zFtoldc". I hope it can be loaded.
Thank you very much.
 
  • #14
So what exactly are you trying to calculate? The particle is labeled as traveling at 6.5km/s (!), which puts it solidly in the hypersonic flow regime, and compressibility will be necessary.
 
  • #15
cjl said:
So what exactly are you trying to calculate? The particle is labeled as traveling at 6.5km/s (!), which puts it solidly in the hypersonic flow regime, and compressibility will be necessary.
I want to get the result of velocity, pressure, and temperature after iteration until reaching steady state and make a simulation using Fortran. But, I don't know whether the illustration of horizontal pipe is correct or not, because it is nonsymmetric. If I illustrate in a half of pipe like the third picture, is it right?
 

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