Characteristics of shock tube generated compressible vortex rings at very high shock Mach numbers
Sajag Poudel, Chandrala Lakshmana Dora, Ashoke De, Debopam Das

TL;DR
This study numerically investigates high Mach number compressible vortex rings generated in shock tubes, including the first simulation of supersonic vortex rings using hydrogen, and highlights the effectiveness of the DES turbulence model in capturing complex vortex phenomena.
Contribution
It reports the first numerical simulation of supersonic vortex rings (Mv > 1) using hydrogen and demonstrates the DES turbulence model's accuracy in replicating experimental vortex characteristics.
Findings
First simulation of supersonic vortex rings with hydrogen.
DES turbulence model accurately predicts vortex features.
High Mach number vortex rings exhibit multiple CRVRs and complex shear layers.
Abstract
Compressible vortex rings, usually formed at the open end of a shock tube, often show interesting phenomena during their formation, evolution, and propagation depending on the shock Mach number (Ms) and exit flow conditions. The Mach number of the translating compressible vortex rings (Mv) investigated so far in the literature is subsonic as, the shock tube pressure ratio (PR) considered is relatively low. In this numerical study we focus on low to high vortex ring Mach numbers (0.31 < Mv < 1.08) cases with a particular focus on very high Mv cases that are not been reported in experiments as, it is difficult to obtain in laboratory. Using hydrogen as a driver section gas inside the shock tube, a supersonic compressible vortex ring (Mv > 1) is obtained for first time. It is established that the SST k-{\omega} based DES turbulent model replicates the experimental observation better than…
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