An analysing
flow pattern in a converging-diverging nozzle has been one of interesting topic
in computational fluid dynamics. There are numerous applications of this flow phenomenon in aerospace and engineering sciences. Such processes are difficult
to handle analytically due to complex mathematical model associated to the flow
and ensuing instabilities carried by flow parameters. Looking back to the
history Jaffery and Hamel, in their studies considered the converging diverging
channel steady two dimensional Newtonian fluid flow.
They observed quiet
interesting results by treating Navier-Stokes equations with similarity
transforms. Further developments were presented in Schlichtinh and Batchelor
based on the boundary layer approximations. Makinde examined the in compressible Newtonian fluid flow by incorporation of linearly diverging symmetrical channel.
Recently, Zarqa et al. performed approximate analytical analysis using Adomian
decomposition method for a channel with variable diverging ratio.
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