Axisymmetric cavities in hypersonic flow
Soumya R. Nanda, T. V. Krishna, S. K. Karthick, J. Cohen

TL;DR
This study investigates the shear layer dynamics of axisymmetric cavities in hypersonic flow at Mach 6, revealing how geometry and Reynolds number influence vortex formation, mode switching, and transition to turbulence.
Contribution
It provides detailed experimental insights into shear layer behavior, mode transitions, and frequency characteristics for various cavity geometries at hypersonic speeds.
Findings
Shear layer remains laminar at low Reynolds numbers and develops vortices as Re increases.
Transition to turbulence occurs at higher Re for longer cavities.
Mode switching depends on rear-face height difference, with pressure build-up influencing dominant modes.
Abstract
A detailed experimental campaign is conducted to investigate the shear layer characteristics of an axisymmetric open cavity exposed to a Mach freestream. Experiments are performed in a Ludwieg tunnel for varying Reynolds numbers () based on cavity depth (). The effects of geometry are examined through length-to-depth ratios () and non-dimensional rear-face height differences (). Shear layer evolution is interpreted using qualitative schlieren and Planar Laser Rayleigh Scattering (PLRS) along with quantitative unsteady pressure measurements. For all , the shear layer remains laminar at low and develops Kelvin-Helmholtz (K-H) vortices as increases. For the longest cavity (), transition to turbulence occurs at the highest due to a longer K-H growth length. Spectral…
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Taxonomy
TopicsFluid Dynamics and Turbulent Flows · Aerodynamics and Acoustics in Jet Flows · Computational Fluid Dynamics and Aerodynamics
