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Batchelor vortex

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Influid dynamics,Batchelor vortices, first described byGeorge Batchelor in a 1964 article, have been found useful in analyses of airplane vortex wake hazard problems.[1][2]

The model

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The Batchelor vortex is an approximate solution to theNavier–Stokes equations obtained using aboundary layer approximation. The physical reasoning behind this approximation is the assumption that the axial gradient of the flow field of interest is of much smaller magnitude than the radial gradient.
The axial, radial and azimuthal velocity components of the vortex are denotedU{\displaystyle U},V{\displaystyle V} andW{\displaystyle W} respectively and can be represented in cylindrical coordinates(x,r,θ){\displaystyle (x,r,\theta )} as follows:

U(r)=U+W0(R/R0)2e(r/R)2,V(r)=0,W(r)=qW01e(r/R)2(r/R0).{\displaystyle {\begin{array}{cl}U(r)&=U_{\infty }+{\frac {W_{0}}{(R/R_{0})^{2}}}e^{-(r/R)^{2}},\\V(r)&=0,\\W(r)&=qW_{0}{\frac {1-e^{-(r/R)^{2}}}{(r/R_{0})}}.\end{array}}}

The parameters in the above equations are


Note that the radial component of the velocity is zero and that the axial and azimuthal components depend only onr{\displaystyle r}.
We now write the system above in dimensionless form by scaling time by a factorR0/W0{\displaystyle R_{0}/W_{0}}. Using the same symbols for the dimensionless variables, the Batchelor vortex can be expressed in terms of the dimensionless variables as

{U(r)=a+11+4t/Reer2/(1+4t/Re),V(r)=0,W(r)=q1er2/(1+4t/Re)r,{\displaystyle \left\lbrace {\begin{array}{cl}U(r)&=a+\displaystyle {{\frac {1}{1+4t/Re}}e^{-r^{2}/(1+4t/Re)}},\\V(r)&=0,\\W(r)&=q\displaystyle {\frac {1-e^{-r^{2}/(1+4t/Re)}}{r}},\end{array}}\right.}

wherea=U/W0{\displaystyle a=U_{\infty }/W_{0}} denotes the free stream axial velocity andRe{\displaystyle Re} is theReynolds number.

If one letsa=0{\displaystyle a=0} and considers an infinitely large swirl number then the Batchelorvortex simplifies to theLamb–Oseen vortex for the azimuthal velocity:

WΘ(r)=Γ2πr(1er2/Rc2){\displaystyle W_{\Theta }(r)={\frac {\Gamma }{2\pi r}}\left(1-e^{-r^{2}/R_{c}^{2}}\right)}

whereΓ{\displaystyle \Gamma } is the circulation.

References

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  1. ^Batchelor, G. K. (1964). Axial flow in trailing line vortices. Journal of Fluid Mechanics, 20(4), 645-658.
  2. ^"Theoretical and numerical analysis of wake vortices"(PDF).ESAIM. Retrieved2015-07-29.

External links

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