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 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 denoted, and respectively and can be represented in cylindrical coordinates as follows:
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 on.
We now write the system above in dimensionless form by scaling time by a factor. Using the same symbols for the dimensionless variables, the Batchelor vortex can be expressed in terms of the dimensionless variables as
where denotes the free stream axial velocity and is theReynolds number.
If one lets and considers an infinitely large swirl number then the Batchelorvortex simplifies to theLamb–Oseen vortex for the azimuthal velocity:
where is the circulation.
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