Graduate How Does Anisotropy Affect the Calculation of Taylor Microscale in Turbulence?

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The Taylor microscale can be calculated for anisotropic turbulence using the modified equation that accounts for anisotropic velocity fluctuations. In cases where two velocity components are zero, the expression simplifies to λ_A = √(5ν/ε)√(v'_1²). This approach remains valid as the anisotropy affects only the magnitude of the fluctuations, not the overall formula. References for further reading include "Anisotropic Turbulence" and "Turbulence: An Introduction for Scientists and Engineers." Understanding these concepts is crucial for accurately analyzing turbulence in various applications.
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Anisotropic Taylor microscale
The Taylor microscale in isotropic turbulence is given by:
$$\lambda = \sqrt{ 15 \frac{\nu \ v'^2}{\epsilon} }$$

where v' is the root mean square of the velocity fluctuations. In general, for velocity fluctuations in three dimensions:

$$v' = \frac{1}{\sqrt{3}}\sqrt{{v'_1}^2+{v'_2}^2+{v'_3}^2}$$

So plugging this expression into the Taylor microscale equation yields:
$$\lambda = \sqrt{ 5 \frac{\nu}{\epsilon} }\sqrt{{v'_1}^2+{v'_2}^2+{v'_3}^2}$$

Now for isotropic turbulence

$$v'_1=v'_2=v'_3$$

So for isotropic turbulence, equation 3 (third equation in this text) yields:

$$\lambda = \sqrt{ 5 \frac{\nu}{\epsilon} }\sqrt{{3v'_1}^2} = \sqrt{ 15 \frac{\nu \ {v'_1}^2}{\epsilon} }$$

My question is: can I use equation 3 to calculate the Taylor microscale for anisotropic turbulence. For example if the injection of energy is highly anisotropic where ##v'_2 = v'_3=0##

$$\lambda_A = \sqrt{ 5 \frac{\nu}{\epsilon} }\sqrt{{v'_1}^2}=\sqrt{ 5 \frac{\nu \ {v'_1}^2}{\epsilon} }$$

where ##λ_A## is the anisotropic Taylor microscale. Does this seem correct? Also, does anyone know of a reference where this derivation was already done?
 
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Yes, you can use equation 3 to calculate the Taylor microscale for anisotropic turbulence as long as you take into account the anisotropy in the velocity fluctuations. In your example, where ##v'_2 = v'_3=0##, the Taylor microscale would be given by:

$$\lambda_A = \sqrt{ 5 \frac{\nu}{\epsilon} }\sqrt{{v'_1}^2+0+0}=\sqrt{ 5 \frac{\nu \ {v'_1}^2}{\epsilon} }$$

This is because the anisotropy in the velocity fluctuations only affects the magnitude of the velocity fluctuations, not the overall expression for the Taylor microscale.

As for references, there are many papers and textbooks that discuss the anisotropic Taylor microscale, such as "Anisotropic Turbulence" by F. Anselmet, Y. Gagne, E. J. Hopfinger, and R. A. Antonia, and "Turbulence: An Introduction for Scientists and Engineers" by P. A. Davidson. You can also find many research papers that use this equation to calculate the anisotropic Taylor microscale in various types of turbulence.
 
Topic about reference frames, center of rotation, postion of origin etc Comoving ref. frame is frame that is attached to moving object, does that mean, in that frame translation and rotation of object is zero, because origin and axes(x,y,z) are fixed to object? Is it same if you place origin of frame at object center of mass or at object tail? What type of comoving frame exist? What is lab frame? If we talk about center of rotation do we always need to specified from what frame we observe?

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