Behaviour of turbulent Prandtl/Schmidt number in compressible mixing layer

Author:

Javed Afroz1,Rajan NKS2,Chakraborty Debasis1

Affiliation:

1. Directorate of Computational Dynamics, Defence Research and Development Laboratory, Kanchanbagh, Hyderabad, India

2. Department of Aerospace Engineering, Indian Institute of Science, Bangalore, India

Abstract

The behaviour of turbulent Prandtl/Schmidt number is explored through the model-free simulation results. It has been observed that compressibility affects the Reynolds scalar flux vectors. Reduced peak values are also observed for compressible convective Mach number mixing layer as compared with the incompressible convective Mach number counterpart, indicating a reduction in the mixing of enthalpy and species. Prt and Sct variations also indicate a reduction in mixing. It is observed that unlike the incompressible case, it is difficult to assign a constant value to these numbers due to their continuous variation in space. Modelling of Prt and Sct would be necessary to cater for this continuous spatial variation. However, the turbulent Lewis number is evaluated to be near unity for the compressible case, making it necessary to model only one of the Prt and Sct..

Publisher

SAGE Publications

Subject

Mechanical Engineering,Aerospace Engineering

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