Batchelor Vortex

 The Batchelor vortex is an approximate solution to the Navier-Stokes equation. The Navier stokes equation is obtained using a boundary layer approximation. The approximation is explained with the physical relations.  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. Batchelor vortex is first termed by George Batchelor. He described the bachelor vortex can be used to analyze the airplane vortex wake hazard problems. The various components are present in the bachelor vortex. the compounds are named as the axial velocity, radial velocity, and azimuthal velocity components.  

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