Published March 25, 2021 | Version Submitted
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Nonlinear input/output analysis: application to boundary layer transition

  • 1. ROR icon California Institute of Technology
  • 2. ROR icon University of Paris-Saclay

Abstract

We extend linear input/output (resolvent) analysis to take into account nonlinear triadic interactions by considering a finite number of harmonics in the frequency domain using the harmonic balance method. Forcing mechanisms that maximise the drag are calculated using a gradient-based ascent algorithm. By including nonlinearity in the analysis, the proposed frequency-domain framework identifies the worst-case disturbances for laminar-turbulent transition. We demonstrate the framework on a flat-plate boundary layer by considering three-dimensional spanwise-periodic perturbations triggered by a few optimal forcing modes of finite amplitude. Two types of volumetric forcing are considered, one corresponding to a single frequency/spanwise wavenumber pair, and a multi-harmonic where a harmonic frequency and wavenumber are also added. Depending on the forcing strategy, we recover a range of transition scenarios associated with K-type and H-type mechanisms, including oblique and planar Tollmien–Schlichting waves, streaks and their breakdown. We show that nonlinearity plays a critical role in optimising growth by combining and redistributing energy between the linear mechanisms and the higher perturbation harmonics. With a very limited range of frequencies and wavenumbers, the calculations appear to reach the early stages of the turbulent regime through the generation and breakdown of hairpin and quasi-streamwise staggered vortices.

Additional Information

© The Author(s), 2021. Published by Cambridge University Press. Received 24 January 2020; revised 1 November 2020; accepted 2 November 2020. We would like to thank U. Rist for providing the details for the boundary conditions used in the DNS (Rist & Fasel 1995). This work was initiated while D.S. was Visiting Associate at Caltech. G.R. and T.C. also acknowledge the support of the Boeing Company through a Strategic Research and Development Relationship Agreement CT-BA-GTA-1. The authors report no conflict of interest.

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Additional details

Additional titles

Alternative title
Non-linear input/output analysis: application to boundary layer transition

Identifiers

Eprint ID
101872
DOI
10.1017/jfm.2020.982
Resolver ID
CaltechAUTHORS:20200311-160934521

Funding

Boeing Company Strategic Research and Development Relationship
CT-BA-GTA-1

Dates

Created
2020-03-11
Created from EPrint's datestamp field
Updated
2021-11-16
Created from EPrint's last_modified field