Laminar Three Dimensional Boundary Layers with Swirl in Slip Flow Regime

Authors

  • A. G. Deshpande Indian Institute of Science, Bangalore
  • C. S. Vimala Indian Institute of Science, Bangalore
  • G. Nath Indian Institute of Science, Bangalore

DOI:

https://doi.org/10.14429/dsj.26.6635

Keywords:

Slightly rarefied gases, Perturbation techniques, Runge Kutta Gill method

Abstract

The effect of slip on swirling, low speed flows of slightly rarefied gases in the slip flow regime in a three dimensional axisymmetric laminar boundary layer is investigated by similarity solution approach and by use of perturbation techniques. The governing ordinary differential equations are solved numerically using Runge-Kutta-Gill method. The results show that the skin friction and the heat transfer are reduced due to the effect of slip.

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Published

2014-07-01

How to Cite

Deshpande, A. G., Vimala, C. S., & Nath, G. (2014). Laminar Three Dimensional Boundary Layers with Swirl in Slip Flow Regime. Defence Science Journal, 26(3), 123–126. https://doi.org/10.14429/dsj.26.6635

Issue

Vol. 26 No. 3

Section

Research Papers

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