This study is aimed at understanding the compressible flow physics when an external shock interacts with the wake behind a circular cylinder using a parametric study. The key parameters in this study are freestream Mach number, Reynolds number and the shock strength (shock angle).
The candidate will conduct high-fidelity numerical simulations and experiments to discover the flow regimes in the identified parametric space.
How to Apply
Express your interest by emailing Dr Krishna Talluru at k.talluru@adfa.edu.au. Include a copy of your CV and your academic transcript(s).
School / Research Area
Engineering and Technology, UNSW Canberra
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