Is Turbulence at Point A Isotropic? Calculation Help

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The discussion revolves around determining whether turbulence at a specific point in a fully developed turbulent pipe flow is isotropic. The participant has calculated two root mean square (rms) values of velocity fluctuations at point A: one parallel to the pipe axis (7.55) and another along the radius (0.335). It is concluded that since these two rms values differ, the turbulence at point A is not isotropic. The conversation also touches on the need to consider a third velocity component, the circumferential direction, for a complete analysis of isotropy. Additionally, there is confusion regarding the calculation of turbulent kinetic energy, emphasizing the importance of distinguishing between velocity components and their fluctuations.
  • #31
((0.0625)(0.3125)+(0.4625)(0.1125)+(0.5624)(-0.2875)+...)/8
 
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  • #32
Chestermiller said:
I don't know how you got that average velocity plot, but it doesn't look right. How did you end up with the funny shape?
For the velocity gradient, I get: (7.8625 - 7.525)/0.8

Chet

I plot the average velocity at A (7.525), where I take A as the origin (0,0). Then I plot average velocity at B (7.5375) which is 0.4mm from A (0.4, 7..5375). Then I plot the average velocity at C (7.8625) at 0.8mm from A (0.8, 7.8625).
I then asked ms excel to generate the equation of the linear line and the gradient for me (0.4219).

Understood, (7.8625 - 7.525)/0.8= 0.421875 is a much simpler way to find the derivative,
Thank you Chet!
 
  • #33
Chestermiller said:
((0.0625)(0.3125)+(0.4625)(0.1125)+(0.5624)(-0.2875)+...)/8
Ah, I see, thank you very much Sir! How clueless of me!
 
  • #34
Chestermiller said:
This is not correct. You don't use the rms values of the fluctuations in the two directions. You use the average of the product of the individual fluctuations in the two directions.

You need to use the average velocities at the points A, B, and C to get the derivative of the average velocity.

No. Not for this.

The viscous shear stress is thus: τ = 1.8 * 10-5 * 0.4219.
I was wondering, for the turbulent shear stress, I consider both the fluctuations in the radial and axial direction.
But for the viscous shear stress I only consider the fluctuations at the axial direction.
Why and when do I have to only consider the viscous shear stress in the axial direction?

upload_2015-10-29_20-36-40.png
,
upload_2015-10-29_20-36-55.png


I also attempt to determine the eddy viscosity at B. I read some book which have rather different formulas for eddy viscosity:
McComb (2003) wrote that -ρ×u1'×u2' = ρ×VT×(dU1/dx2) (this book only considers one direction, I don't know why), where VT is the kinematic eddy viscosity.

Pope (2000) wrote that -ρ×u1'×u2' + 2/3 ×ρ×κ×δ12 = ρ×VT×(dU1/dx2)×(dU2/dx1) (this book considers two directions), where κ is the kinetic energy, δ is the Kronecker delta (I'm not sure what it is), VT is the eddy viscosity (without kinematic).

And this lecture online (http://www.bakker.org/dartmouth06/engs150/10-rans.pdf) says that:

upload_2015-10-29_20-52-40.png


where the μt is the eddy viscosity and kinematic turbulent viscosity is actually VT = μt/ρ.

I'm really confused on which equation I should chose and do I have to consider the kinetic energy and kronecker delta to determine the eddy viscosity?
Why does Pope (2000) states that VT is the eddy viscosity (without kinematic) while McComb (2003) states that VT is the kinematic turbulent viscosity?

Thank you very much for the guidance all this time.
 
  • #35
nightingale said:
The viscous shear stress is thus: τ = 1.8 * 10-5 * 0.4219.
I was wondering, for the turbulent shear stress, I consider both the fluctuations in the radial and axial direction.
But for the viscous shear stress I only consider the fluctuations at the axial direction.
Why and when do I have to only consider the viscous shear stress in the axial direction?
Both the viscous stress and the turbulent stress you calculated are on a surface of constant r in the z direction, but also on a surface of constant z in the r direction.
View attachment 90985, View attachment 90986

I also attempt to determine the eddy viscosity at B. I read some book which have rather different formulas for eddy viscosity:
McComb (2003) wrote that -ρ×u1'×u2' = ρ×VT×(dU1/dx2) (this book only considers one direction, I don't know why), where VT is the kinematic eddy viscosity.

Pope (2000) wrote that -ρ×u1'×u2' + 2/3 ×ρ×κ×δ12 = ρ×VT×(dU1/dx2)×(dU2/dx1) (this book considers two directions), where κ is the kinetic energy, δ is the Kronecker delta (I'm not sure what it is), VT is the eddy viscosity (without kinematic).

And this lecture online (http://www.bakker.org/dartmouth06/engs150/10-rans.pdf) says that:

View attachment 90987

where the μt is the eddy viscosity and kinematic turbulent viscosity is actually VT = μt/ρ.

I'm really confused on which equation I should chose and do I have to consider the kinetic energy and kronecker delta to determine the eddy viscosity?
Why does Pope (2000) states that VT is the eddy viscosity (without kinematic) while McComb (2003) states that VT is the kinematic turbulent viscosity?

Thank you very much for the guidance all this time.
Your questions are indicating that your fundamental understanding of turbulence and turbulent stresses needs beefing up. You need to understand the fundamentals before you start trying to apply it to problems. I'm going to recommend another book that I hold in high regard, and hope you will consider using it: Transport Phenomena by Bird, Stewart, and Lightfoot, Chapter 5. Physics Forums is just not structured to present a complete primer on Turbulent Flow.

Chet
 
  • #36
Chestermiller said:
Both the viscous stress and the turbulent stress you calculated are on a surface of constant r in the z direction, but also on a surface of constant z in the r direction.

Your questions are indicating that your fundamental understanding of turbulence and turbulent stresses needs beefing up. You need to understand the fundamentals before you start trying to apply it to problems. I'm going to recommend another book that I hold in high regard, and hope you will consider using it: Transport Phenomena by Bird, Stewart, and Lightfoot, Chapter 5. Physics Forums is just not structured to present a complete primer on Turbulent Flow.

Chet

Thank you Sir.

I have borrowed the book you recommend and read chapter 5 and chapter 1 which talk about kronecker delta. I really helps me to understand turbulence better.
I'm still intrigued on why Pope (2000) simply said VT as 'eddy viscosity' when it is, I think, 'kinematic eddy viscosity' but I decided I'll ask my teacher next time I met her.

I now know that the formula I should be using is:

-ρu'v' = μT * dU/dy

Where the μT here is the eddy viscosity.

Earlier the turbulent shear stress is:
τ = -ρu'v'
τ = - 1.2 * ((0.0625)(0.3125)+(0.4625)(0.1125)+(0.5624)(-0.2875)+...)/8
τ = 0.11343

and the velocity gradient is 0.4219

Thus the eddy viscosity is:
0.11343 = μ * 0.4219
μ = 0.27
Did I do right? Thank you very much.
 
  • #37
nightingale said:
Thank you Sir.

I have borrowed the book you recommend and read chapter 5 and chapter 1 which talk about kronecker delta. I really helps me to understand turbulence better.
I'm still intrigued on why Pope (2000) simply said VT as 'eddy viscosity' when it is, I think, 'kinematic eddy viscosity' but I decided I'll ask my teacher next time I met her.

I now know that the formula I should be using is:

-ρu'v' = μT * dU/dy

Where the μT here is the eddy viscosity.

Earlier the turbulent shear stress is:
τ = -ρu'v'
τ = - 1.2 * ((0.0625)(0.3125)+(0.4625)(0.1125)+(0.5624)(-0.2875)+...)/8
τ = 0.11343

and the velocity gradient is 0.4219

Thus the eddy viscosity is:
0.11343 = μ * 0.4219
μ = 0.27
Did I do right? Thank you very much.
Yes. But please make sure the you show the units.
 
  • #38
Chestermiller said:
Yes. But please make sure the you show the units.

Thank you, Sir. I take the unit of the eddy viscosity as Pa.s.

I attempt to do the last question, which asked me to determine the production of the turbulence energy at B.
I found that the corresponding formula is:

Production = -2 u'v'*(dU/dy)
and thus the production is:
Production = -2 *((0.0625)(0.3125)+(0.4625)(0.1125)+(0.5624)(-0.2875)+...)/8 * (0.4219)
Production = -2 * -0.094525 * 0.4219
Production = 0.0798

Did I do it correctly?
Thank you very much for the guidance.
 
  • #39
I can't help you here. I'm not familiar with the equation you wrote for the rate of production of turbulent energy. But, it doesn't seem to have the right units.

Chet
 
  • #40
Chestermiller said:
I can't help you here. I'm not familiar with the equation you wrote for the rate of production of turbulent energy. But, it doesn't seem to have the right units.

Chet

I understand, I will continue to read about the topic. Thank you very much for the patience and the guidance all this time Chet! You are a wonderful teacher!
 

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