Laminar Three Dimensional Boundary Layers with Swirl in Slip Flow Regime

  • A. G. Deshpande Indian Institute of Science, Bangalore
  • C. S. Vimala Indian Institute of Science, Bangalore
  • G. Nath Indian Institute of Science, Bangalore
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.
Published
2014-07-01
How to Cite
Deshpande, A., Vimala, C., & 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
Section
Research Papers