Exploration of supersonic confined mixing layer: Effect of dissimilar gases at different temperatures

Author:

Javed Afroz1,Paul PJ2,Rajan NKS2,Chakraborty Debasis1

Affiliation:

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

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

Abstract

The growth rate of high-speed mixing layer between two dissimilar gases is explored through the model free simulation results. To analyse the cause for the higher mixing layer growth rate in comparison to the existing values reported in literature, the results were compared with the model free simulations of mixing of two high-speed streams of nitrogen (similar gas) at matched temperature and density. The analysis indicates that pressure and density fluctuations no longer remain correlated completely for the mixing layer formed between two dissimilar gases at different temperatures in contrast to the complete pressure density correlation for similar gases. It has been observed that the correlation between temperature and density fluctuations is near −1.0 for dissimilar gases in the mixing layer region and is much higher than for similar gases. It is concluded that mixing layer of similar gases shows a decrease in growth rate due to compressibility effect, while that of dissimilar gases shows a decrease due to dominant temperature effect on density.

Publisher

SAGE Publications

Subject

Mechanical Engineering,Aerospace Engineering

Cited by 3 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Stability analysis of shock-mixing interaction based on dynamic mode decomposition;Aerospace Science and Technology;2022-04

2. Numerical study of unsteady shock/mixing interaction in confined space;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2022-03-09

3. Reynolds averaged Navier-Stokes simulations of compressible mixing layers of similar and dissimilar gases: Performance of k–ɛ turbulence model;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2014-11-12

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