Jet-edge interaction: linear and non-linear frequency-selection mechanisms

TL;DR

This study investigates the spectral signatures and underlying mechanisms of jet-edge interactions, revealing linear and non-linear frequency-selection regimes, mode-switching phenomena, and their dependence on jet Mach number and plate position.

Contribution

It classifies spectral regimes and identifies mechanisms behind regime changes, including linear, non-linear, and mode-switching phenomena in jet-edge interactions.

Findings

Identification of linear and non-linear frequency-selection regimes.

Discovery of a robust mode-switching mechanism at Mach 0.84.

Observation of triadic interactions and harmonic generation in spectral regimes.

Abstract

We consider a round turbulent jet grazing a rectangular plate angled at $45^\circ$. Through sound pressure measurements, the tonal dynamics associated with jet-edge interaction are explored in a parameter space comprising jet Mach number, $M_j$, and plate radial position, $R/D$. A variety of spectral signatures are observed and classified. The classification - based on analysis of power-spectral density and bicoherence, and on the resonance model proposed by Jordan et al. (2018) - comprises: broadband spectra; tonal spectra associated with purely linear frequency-selection mechanisms; tonal spectra associated with both linear and non-linear frequency selection. The classification identifies regions in the parameter space ($M_j$, $R/D$); and clarifies mechanisms underpinning regime changes. The linear frequency selection (LFS) regime comprises multiple tones, with no evidence of triad interaction. A regime involving non-linear frequency selection emerges from this state, with the strong amplification of one LFS tone, which then generates multiple harmonics. Intermediate regimes are identified involving weaker, non-harmonic triadic interactions where two LFS tones interact to generate a third tone. In addition to these mechanisms a mode-switching mechanism is identified at $M_j$ = 0.84 and shown to result from the cut-on of a new upstream-travelling wave at that Mach number. The mode-switch is found to be remarkably robust, occurring in a repeatable manner over a Mach-number increment of 0.01 regardless of whether the Mach number is increased or decreased (no hysteresis is observed).