4.7 Article

Low-frequency resolvent analysis of the laminar oblique shock wave/boundary layer interaction

Journal

JOURNAL OF FLUID MECHANICS
Volume 942, Issue -, Pages -

Publisher

CAMBRIDGE UNIV PRESS
DOI: 10.1017/jfm.2022.390

Keywords

boundary layer separation; boundary layer receptivity; shock waves

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Resolvent analysis is used to study the low-frequency behavior of the laminar oblique shock wave/boundary layer interaction (SWBLI). The computed optimal gain follows a first-order low-pass filter equation, consistent with previous findings. The damping rate scales with the scale, resulting in a constant Strouhal number. The study supports the idea that the low-frequency dynamics of the SWBLI is a forced dynamics, with background perturbations continuously exciting the flow.
Resolvent analysis is used to study the low-frequency behaviour of the laminar oblique shock wave/boundary layer interaction (SWBLI). It is shown that the computed optimal gain, which can be seen as a transfer function of the system, follows a first-order low-pass filter equation, recovering the results of Touber & Sandham (J. Fluid Mech., vol. 671, 2011, pp. 417-465). This behaviour is understood as proceeding from the excitation of a single stable, steady global mode whose damping rate sets the time scale of the filter. Different Mach and Reynolds numbers are studied, covering different recirculation lengths . This damping rate is found to scale as , leading to a constant Strouhal number as observed in the literature. It is associated with a breathing motion of the recirculation bubble. This analysis furthermore supports the idea that the low-frequency dynamics of the SWBLI is a forced dynamics, in which background perturbations continuously excite the flow. The investigation is then carried out for three-dimensional perturbations for which two regimes are identified. At low wavenumbers of the order of , a modal mechanism similar to that of two-dimensional perturbations is found and exhibits larger values of the optimal gain. At larger wavenumbers, of the order of the boundary layer thickness, the growth of streaks, which results from a non-modal mechanism, is detected. No interaction with the recirculation region is observed. Based on these results, the potential prevalence of three-dimensional effects in the low-frequency dynamics of the SWBLI is discussed.

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