Abstract

Comprehensive experimental and computational investigations have revealed possible mechanisms underlying low-frequency unsteadiness observed in spanwise homogeneous shock-wave/turbulent-boundary-layer interactions (STBLI). In the present work, we extend this understanding by examining the dynamic linear response of a moderately separated Mach 2.3 STBLI to small perturbations. The statistically stationary linear response is analysed to identify potential time-local and time-mean linear tendencies present in the unsteady base flow: these provide insight into the selective amplification properties of the flow at various points in the limit cycle, as well as asymmetry and restoring mechanisms in the dynamics of the separation bubble. The numerical technique uses the synchronized large-eddy simulation method, previously developed for free shear flows, significantly extended to include a linear constraint necessary for wall-bounded flows. The results demonstrate that the STBLI fosters a global absolute linear instability corresponding to a time-mean linear tendency for upstream shock motion. The absolute instability is maintained through constructive feedback of perturbations through the recirculation: it is self-sustaining and insensitive to external forcing. The dynamics are characterized for key frequency bands corresponding to high–mid-frequency Kelvin–Helmholtz shedding along the separated shear layer$(St_{L}\sim 0.5)$, low–mid-frequency oscillations of the separation bubble$(St_{L}\sim 0.1)$and low-frequency large-scale bubble breathing and shock motion$(St_{L}\sim 0.03)$, where the Strouhal number is based on the nominal length of the separation bubble,$L$:$St_{L}=fL/U_{\infty }$. A band-pass filtering decomposition isolates the dynamic flow features and linear responses associated with these mechanisms. For example, in the low-frequency band, extreme shock displacements are shown to correlate with time-local linear tendencies toward more moderate displacements, indicating a restoring mechanism in the linear dynamics. However, a disparity between the linearly stable shock position and the mean shock position leads to an observed asymmetry in the low-frequency shock motion cycle, in which upstream motion occurs more rapidly than downstream motion. This is explained through competing linear and nonlinear (mass depletion through shedding) mechanisms and discussed in the context of an oscillator model. The analysis successfully illustrates how time-local linear dynamics sustain several key unsteady broadband flow features in a causal manner.

Highlights

  • This technique for analysing flow stability may be classified as global (Theofilis 2011), as opposed to local (Huerre & Monkewitz 1990), and non-modal (Schmid 2007), as opposed to modal (Schmid & Henningson 2001), following terminology described in the aforementioned references; it considers the global influence of the flow, and no ansatz of frequency-isolated modes is assumed, since intermodal frequency mixing will generally occur for linear perturbations of an unsteady base flow; such an occurrence may arise without any nonlinear interactions

  • These observations are connected to the concepts of absolute and convective global instabilities discussed by Huerre & Monkewitz (1990) and Chomaz (2005), which we observe in the Shock-wave/turbulent-boundary-layer interactions (STBLI) and undisturbed turbulent boundary layer, respectively; in response to forcing, absolutely unstable flows exhibit self-sustained oscillations, whereas convectively unstable flows respond as selective amplifiers

  • We discuss in § 5.3.6 the band-isolated dynamics of the base flow and perturbations in the context of a mass-depletion mechanism, e.g. the conceptual model of Piponniau et al (2009). Such a model is consistent with the low-frequency dynamics; like Morgan et al (2013) we find that the ‘turbulent separation bubble’ responds more significantly at higher frequencies (StL ∼ 0.1) than predicted by the model (StL ∼ 0.03)

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Summary

General overview

Shock-wave/turbulent-boundary-layer interactions (STBLI) occur in many high-speed applications such as air intakes, control surfaces and over-expanded nozzles. This work was a natural extension of an earlier effort by Touber & Sandham (2009), who perturbed the time-mean flow obtained from an LES of a turbulent SBLI using white noise to find an unstable, two-dimensional, global mode with a growth time scale similar to that observed in low-frequency bubble breathing. They corroborated their findings with a BiGlobal linear-stability analysis of the time-mean turbulent flow, which, in addition to an unstable non-oscillatory (zero-frequency) global mode, identified several weakly damped oscillatory modes resembling bubble breathing extracted from low-pass filtered LES flow fields This analysis was extended by Nichols et al (2017) who describe the STBLI as a weakly damped oscillator, sustained by forcing, with a non-oscillatory unstable global mode. A unified theoretical basis for linearizing propagation equations about a steady base flow that is not a steady solution to the given propagation equations remains to be developed

Current contribution
Dynamic linear response
Application to STBLI
Theoretical and numerical model
Constrained linearization technique
Governing equations of dynamic linear response
Forcing term Two independent forms of the forcing term S are considered
Constraining term
Synchronized LES
Relationship between constrained and unconstrained perturbations
Description of STBLI base-flow simulation
Forcing parameters and cases considered
Analysis of transient amplification of unconstrained perturbation field
Analysis of statistically stationary linearly constrained perturbation field
Linearity of constrained perturbation field
Spectral content of base-flow and perturbation fields
Conclusions
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