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B Model Functions for Size Distributions

Note that we could not have derived (2.1.2) by letting C equal zero in (2. A.8) since the viscosity /x was assumed to be nonzero to arrive at (2. A.8) in the first place. [Pg.41]

In the same way that (2.A.7) was derived from the 0-component equation of (2.A.2), two other differential equations for the flow field in a vortex motion can be derived from the r- and the 2 -component equations. They are, respectively  [Pg.41]

Equation (2.A.12) is the balance between the centrifugal force (or the mass times the centripetal acceleration) and the pressure force, all on a per unit volume basis. It shows, as we also saw on basis of heuristic arguments in the main text, that the pressure in a vortex flow increases towards the periphery and more so the stronger the tangential velocity. The radial pressure distribution can be obtained by integrating the right-hand side over r. [Pg.41]

Equation (2.A.13) simply says that the axial pressure distribution is the hydrostatic pressure, which in gas cyclones is not very interesting, since the fluid density is low. [Pg.41]

This completes the derivation of the basic equations for swirling flows from the Navier-Stokes equations. When deriving flow equations, particularly in cylindrical coordinates, this method is safer than using heuristic arguments. [Pg.41]


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