Linear response analysis of supersonic turbulent channel flows with a large parameter space
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 …
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 …
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 …
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 …
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 …
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
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 …
with/without wall cooling is examined with the linear resolvent operator in a compressible …
Structured input-output analysis of compressible plane Couette flow
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 …
recently introduced structured input-output analysis method for incompressible flows to the …
Eddy-viscosity-improved resolvent analysis of compressible turbulent boundary layers
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 …
boundary layers. To better model nonlinear processes in the input, the resolvent framework …
Structured input-output analysis of turbulent flows over riblets
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 …
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
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 …
close to walls. In particular, we study the near-wall asymptotic behavior for adiabatic and …