Analysis of amplification mechanisms and cross-frequency interactions in nonlinear flows via the harmonic resolvent

TL;DR

This paper introduces a harmonic resolvent framework to analyze nonlinear flow dynamics, capturing cross-frequency interactions and energy transfer mechanisms in complex, time-varying flows.

Contribution

It develops a frequency-domain analysis method for periodically time-varying flows, extending resolvent analysis to include triadic interactions and cross-frequency coupling.

Findings

Harmonic resolvent captures triadic interactions in nonlinear flows.

The method reveals space-time amplification modes.

Application examples include ODE systems and airfoil flow at stall.

Abstract

We propose a framework that elucidates the input-output characteristics of flows with complex dynamics arising from nonlinear interactions between different time scales. More specifically, we consider a periodically time-varying base flow, and perform a frequency-domain analysis of periodic perturbations about this base flow; the response of these perturbations is governed by the harmonic resolvent, which is a linear operator similar to the harmonic transfer function introduced by Wereley (1991). This approach makes it possible to explicitly capture the triadic interactions that are responsible for the energy transfer between different time scales in the flow. For instance, perturbations at frequency $\alpha$ are coupled with perturbations at frequency $\omega$ through the base flow at frequency $\omega-\alpha$. We draw a connection with resolvent analsyis, which is a special case of the harmonic resolvent when evaluated about a steady base flow. We show that the left and right singular vectors of the harmonic resolvent are the optimal response and forcing modes, which can be understood as full spatio-temporal signals that reveal space-time amplification characteristics of the flow. We illustrate the method on examples, including a three-dimensional system of ordinary differential equations and the flow over an airfoil at near-stall angle of attack.