Axisymmetric cavities in hypersonic flow
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 analysis of pressure signals and PLRS intensity shows a shift in dominant frequency from the first Rossiter mode to higher modes for . Except for , dominant frequencies agree with Rossiter predictions and remain largely Reynolds-number independent. Variation of leads to mode switching identified using POD of PLRS snapshots. Negative favors K-H modes (5th-6th Rossiter), whereas positive values promote a strong flapping mode (1st Rossiter) due to pressure build-up inside the cavity. At , both modes may coexist depending on . Azimuthal measurements indicate dominant axisymmetric behavior in flapping cases and weaker correlation for K-H dominated shear layers.
Keywords
Cite
@article{arxiv.2602.16663,
title = {Axisymmetric cavities in hypersonic flow},
author = {Soumya R. Nanda and T. V. Krishna and S. K. Karthick and J. Cohen},
journal= {arXiv preprint arXiv:2602.16663},
year = {2026}
}
Comments
18 Figures. Relevant multimedia views and supplementary videos are embedded in the pdf itself. The article is yet to be submitted to a journal