Linear response analysis of supersonic turbulent channel flows with a large parameter space

X Chen, C Cheng, L Fu, J Gan - Journal of Fluid Mechanics, 2023 - cambridge.org
In this work, the linear responses of turbulent mean flow to both harmonic and stochastic
forcing are investigated for supersonic channel flow. Well-established universal relations are …

Wavelet-based resolvent analysis of non-stationary flows

E Ballouz, B Lopez-Doriga, STM Dawson… - Journal of Fluid …, 2024 - cambridge.org
This work introduces a formulation of resolvent analysis that uses wavelet transforms rather
than Fourier transforms in time. Under this formulation, resolvent analysis may extend to …

Subsonic and supersonic mechanisms in compressible turbulent boundary layers: a perspective from resolvent analysis

A Madhusudanan, BJ McKeon - arXiv preprint arXiv:2209.14223, 2022 - arxiv.org
In this study we isolate the mechanisms that are separately responsible for amplifying the
two distinct sets of modes that appear in a linearized Navier-Stokes based model for …

Wavelet-based resolvent analysis for statistically-stationary and temporally-evolving flows

E Ballouz, B Lopez-Doriga, ST Dawson… - AIAA SCITECH 2023 …, 2023 - arc.aiaa.org
View Video Presentation: https://doi. org/10.2514/6.2023-0676. vid This work introduces a
formulation of resolvent analysis that uses wavelet transforms rather than Fourier transforms …

Prediction of resolvent mode shapes in supersonic turbulent boundary layers

STM Dawson, BJ McKeon - International Journal of Heat and Fluid Flow, 2020 - Elsevier
This work applies resolvent analysis to compressible zero-pressure-gradient turbulent
boundary layers with freestream Mach numbers between 2 and 4, focusing exclusively on …

Resolvent-based analysis of hypersonic turbulent boundary layers with/without wall cooling

Y Fan, W Li, RD Sandberg - Physics of Fluids, 2023 - pubs.aip.org
The ability of the low-rank approximation of hypersonic turbulent boundary layers
with/without wall cooling is examined with the linear resolvent operator in a compressible …

Structured input-output analysis of compressible plane Couette flow

D Bhattacharjee, T Mushtaq, PJ Seiler… - AIAA SCITECH 2023 …, 2023 - arc.aiaa.org
View Video Presentation: https://doi. org/10.2514/6.2023-1984. vid This paper extends the
recently introduced structured input-output analysis method for incompressible flows to the …

Eddy-viscosity-improved resolvent analysis of compressible turbulent boundary layers

Y Fan, M Kozul, W Li, RD Sandberg - Journal of Fluid Mechanics, 2024 - cambridge.org
An improved resolvent analysis is proposed in the regime of compressible turbulent
boundary layers. To better model nonlinear processes in the input, the resolvent framework …

Structured input-output analysis of turbulent flows over riblets

T Mushtaq, M Luhar, M Hemati - AIAA AVIATION 2023 Forum, 2023 - arc.aiaa.org
View Video Presentation: https://doi. org/10.2514/6.2023-3446. vid This paper applies
structured input-output (I/O) methods to analyze turbulent channel flows over riblets …

Mach number and wall thermal boundary condition effects on near-wall compressible turbulence

A Baranwal, DA Donzis, RDW Bowersox - arXiv preprint arXiv:2307.03265, 2023 - arxiv.org
We investigate the effects of thermal boundary conditions and Mach number on turbulence
close to walls. In particular, we study the near-wall asymptotic behavior for adiabatic and …