Nonlinear input-output analysis of laminar-turbulent transition for wall-bounded flows

ORAL

Abstract

In a linear input-output analysis framework, the most amplified instabilities are typically described by considering singular vectors of the resolvent operator of the linearized Navier-Stokes equations. In this study, we extend the methodology to take into account nonlinear triadic interactions by considering a finite number of harmonics in the frequency domain using the Harmonic Balance Method. Optimal nonlinear forcing mechanisms that lead to transition and maximize the skin-friction coefficient are identified using direct-adjoint looping. We demonstrate the framework on a zero-pressure flat-plate boundary layer by considering three-dimensional perturbations triggered by a few optimal forcing modes of finite amplitude. Depending on the frequency, spanwise wavenumber, amplitude and symmetries of the perturbation, we recover all the transition stages associated with K-type and H-type transition mechanisms, oblique waves, streaks, and their breakdown. The proposed frequency-domain framework identifies the worst-case frequency disturbances for wall-bounded laminar-turbulent transition.

*G.R. and T.C. acknowledge support from The Boeing Company (CT-BA-GTA-1)

Authors

  • Georgios Rigas

    • Caltech
    • California Institute of Technology
    • Imperial College London
  • Denis Sipp

    • ONERA
    • ONERA - The French Aerospace Lab
    • ONERA, France
  • Tim Colonius

    • California Institute of Technology
    • Caltech