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Laminar boundary layer of gas particulate flow on a flat plate

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Proceedings of the Indian Academy of Sciences - Section A. Part 3, Mathematical Sciences Aims and scope Submit manuscript

Abstract

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.

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Authors and Affiliations

  1. Department of Mathematics, Indian Institute of Technology, 208 016, Kanpur

    Saroj Prabha

  2. Department of Aeronautical Engineering, Indian Institute of Technology, 208 016, Kanpur

    Saroj Prabha & A C Jain

Authors
  1. Saroj Prabha
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  2. A C Jain
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Prabha, S., Jain, A.C. Laminar boundary layer of gas particulate flow on a flat plate. Proc. Indian Acad. Sci. (Math. Sci.) 88, 377–385 (1979). https://doi.org/10.1007/BF03047133

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  • DOI: https://doi.org/10.1007/BF03047133

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