Gas particulate boundary layer equations with no pressure gradient are computed numerically in the physical plane by a Crank-Nicholson scheme of finite differences. Results so obtained are compared with the approximate method of Tabakoff and Hamed. The present analysis gives accurate description of the structure of the boundary layer of the gas particulate flow. A parametric study giving the effect of the changes in the non-dimensional parameter$$\bar F$$ on the various characteristics of the flow is also carried out.
Volume 131, 2021
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