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 6 freestream. Experiments are performed in a Ludwieg tunnel for varying Reynolds numbers (23000≤ ReD ≤ 74000) based on cavity depth (D). The effects of geometry are examined through length-to-depth ratios ([L/D]=[2,4,6]) and non-dimensional rear-face height differences ([ h/D]=[-0.5,-0.25,0,0.25,0.5]). Shear layer evolution is interpreted using qualitative schlieren and Planar Laser Rayleigh Scattering (PLRS) along with quantitative unsteady pressure measurements. For all [L/D], the shear layer remains laminar at low ReD and develops Kelvin-Helmholtz (K-H) vortices as ReD increases. For the longest cavity ([L/D]=6), transition to turbulence occurs at the highest ReD 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 [L/D]=6. Except for [L/D]=6, [ h/D]=0, dominant frequencies agree with Rossiter predictions and remain largely Reynolds-number independent. Variation of [ h/D] leads to mode switching identified using POD of PLRS snapshots. Negative [ h/D] 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 [ h/D]=0, both modes may coexist depending on ReD. Azimuthal measurements indicate dominant axisymmetric behavior in flapping cases and weaker correlation for K-H dominated shear layers.

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