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Master1022
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- What is the purpose of the Prandtl mixing method and what does it mean?
Hi,
I was recently learning about turbulent boundary layers and came across the 'Prandtl mixing length'. I am struggling to understand what the concept is and what its purpose is. I would appreciate any help or guidance of where I can look to gain a better understanding.
The information I currently know is below.
The turbulent 2D boundary layer momentum equation is given by:
Then we can define an eddy viscosity [itex] \epsilon_{M} [/itex] such that:
[tex] \tau_{turbulent} = - \rho \overline{u' v'} = \rho \epsilon_{M} \frac{du}{dy} [/tex]
The cyclic motion of a turbulent packet of fluid results in a turbulent shear stress. Therefore, we seek some model to relate this motion to eddy viscosity. Prandtl postulated that the turbulent fluctuation [itex] u' [/itex] is proportional to the time average of the absolute value of these fluctuations, thus giving:
[tex] u' = l' \frac{du}{dy} [/tex]
This distance [itex] l [/itex] is called Prandtl’s mixing length. Also the idea that [itex] u' [/itex] would be the same order of magnitude as [itex] v′ [/itex] (assumption only valid for isotropic turbulence). Giving:
[tex] \tau_{turbulent} = - \rho \overline{u' v'} = \rho \epsilon_{M} \frac{du}{dy} = \rho l^2 \left( \frac{du}{dy} \right)^2 [/tex]
The eddy viscosity varies through the boundary layer. Prandtl’s hypothesis was that the mixing length is proportional to the distance from the wall, [itex] l = ky [/itex] where [itex] k [/itex] is a constant and also the shear stress is uniform and approximately equal to the value at the wall in the region close to the wall, [itex] \tau_t = \tau_w [/itex]. This leads to an expression for the shear stress
[tex] \tau_t = \rho k^2 y^2 \left( \frac{du}{dy} \right)^2 [/tex]
[itex] y [/itex] is the upper bound of [itex] l [/itex] since mixing length cannot be greater than the distance from the wall by our definition. Taking the square root and integrating gives:
That is the text that I have on the topic. After reading this, I am not completely sure what the purpose of this concept is.
Thanks in advance.
I was recently learning about turbulent boundary layers and came across the 'Prandtl mixing length'. I am struggling to understand what the concept is and what its purpose is. I would appreciate any help or guidance of where I can look to gain a better understanding.
The information I currently know is below.
The turbulent 2D boundary layer momentum equation is given by:
Then we can define an eddy viscosity [itex] \epsilon_{M} [/itex] such that:
[tex] \tau_{turbulent} = - \rho \overline{u' v'} = \rho \epsilon_{M} \frac{du}{dy} [/tex]
The cyclic motion of a turbulent packet of fluid results in a turbulent shear stress. Therefore, we seek some model to relate this motion to eddy viscosity. Prandtl postulated that the turbulent fluctuation [itex] u' [/itex] is proportional to the time average of the absolute value of these fluctuations, thus giving:
[tex] u' = l' \frac{du}{dy} [/tex]
This distance [itex] l [/itex] is called Prandtl’s mixing length. Also the idea that [itex] u' [/itex] would be the same order of magnitude as [itex] v′ [/itex] (assumption only valid for isotropic turbulence). Giving:
[tex] \tau_{turbulent} = - \rho \overline{u' v'} = \rho \epsilon_{M} \frac{du}{dy} = \rho l^2 \left( \frac{du}{dy} \right)^2 [/tex]
The eddy viscosity varies through the boundary layer. Prandtl’s hypothesis was that the mixing length is proportional to the distance from the wall, [itex] l = ky [/itex] where [itex] k [/itex] is a constant and also the shear stress is uniform and approximately equal to the value at the wall in the region close to the wall, [itex] \tau_t = \tau_w [/itex]. This leads to an expression for the shear stress
[tex] \tau_t = \rho k^2 y^2 \left( \frac{du}{dy} \right)^2 [/tex]
[itex] y [/itex] is the upper bound of [itex] l [/itex] since mixing length cannot be greater than the distance from the wall by our definition. Taking the square root and integrating gives:
Thanks in advance.