The effect of Mach number on open cavity flows with thick or thin incoming boundary layers
Marlon Sproesser Mathias, Marcello Augusto Faraco de Medeiros

TL;DR
This study investigates how Mach number influences the stability and flow dynamics of open cavity flows with different boundary layer thicknesses, revealing complex interactions between compressibility, Rossiter modes, and nonlinear effects.
Contribution
It provides a comprehensive analysis combining global linear stability and nonlinear simulations to understand Mach effects on cavity flow instabilities, highlighting the role of acoustic feedback and mode interactions.
Findings
Compressibility destabilizes low Mach flows significantly.
Higher order Rossiter modes become unstable with thin boundary layers.
Nonlinear simulations show dominant frequencies align with R1 mode and empirical predictions.
Abstract
The Rossiter modes of an open cavity were studied using global linear analysis and nonlinear numerical simulations. The length over depth ratio was two and the Reynolds numbers based on cavity depth were close to 1000. The effect of Mach on such cavities was studied. The global analysis revealed that, in the Mach range 0.1 to 0.9, for thick boundary layers, only R1 and R2 modes could become unstable, whereas for thin boundary layer up to R4 could be unstable. Compressibility was very destabilizing at low Mach. At moderate Mach the instability either saturated with Mach or had an irregular dependence. Analysis of the Rossiter mode eigenfunctions indicated that the acoustic feedback scaled to Ma^3, and explained the strong destabilizing effect of compressibility. The irregular dependence was associated with resonances between Rossiter modes and acoustic cavity modes. The analysis…
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