Exploration of supersonic confined mixing layer: Effect of dissimilar gases at different temperatures
Author:
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
Publisher
SAGE Publications
Subject
Mechanical Engineering,Aerospace Engineering
Link
http://journals.sagepub.com/doi/pdf/10.1177/0954410013513680
Reference23 articles.
1. An experimental investigation of the properties of a non-reacting, supersonic shear layer
2. The compressible turbulent shear layer: an experimental study
3. On the density ratio effect on the growth rate of a compressible mixing layer
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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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