activity
20152026
most citedSpectral analysis of jet turbulence

483 citations · 1k across the 21 of their papers we have counts for

collaborators

22 papers

physics.flu-dyn2026

Optimal non-linear mechanisms for laminar-turbulent transition of a shock-induced separated shear layer

Flavio Savarino, Denis Sipp, Georgios Rigas

Laminar-turbulent transition in shock wave-boundary-layer interactions (SWBLI) remains a major challenge for hypersonic vehicle design, with implications for drag, heat transfer, a…

physics.flu-dyn2025★ 1 cited

Optimal transitional mechanisms of incompressible separated shear layers subject to external disturbances

Flavio Savarino, Denis Sipp, Georgios Rigas

Optimal transitional mechanisms are analysed for an incompressible shear layer developing over a short, pressure gradient-induced laminar separation bubble (LSB) with peak reversed…

physics.flu-dyn2023★ 3 cited

RONAALP: Reduced-Order Nonlinear Approximation with Active Learning Procedure

Clément Scherding, Georgios Rigas, Denis Sipp +2

Many engineering applications rely on the evaluation of expensive, non-linear high-dimensional functions. In this paper, we propose the RONAALP algorithm (Reduced Order Nonlinear A…

cs.LG2023★ 2 cited

Mori-Zwanzig latent space Koopman closure for nonlinear autoencoder

Priyam Gupta, Peter J. Schmid, Denis Sipp +2

The Koopman operator presents an attractive approach to achieve global linearization of nonlinear systems, making it a valuable method for simplifying the understanding of complex…

physics.flu-dyn2023★ 1 cited

Active Flow Control for Bluff Body Drag Reduction Using Reinforcement Learning with Partial Measurements

Chengwei Xia, Junjie Zhang, Eric C. Kerrigan +1

Active flow control for drag reduction with reinforcement learning (RL) is performed in the wake of a 2D square bluff body at laminar regimes with vortex shedding. Controllers para…

physics.flu-dyn2023★ 1 cited

Adjoint-based linear sensitivity of a hypersonic boundary layer to steady wall blowing-suction/heating-cooling

Arthur Poulain, Cédric Content, Georgios Rigas +2

For a Mach 4.5 flat-plate adiabatic boundary layer, we study the sensitivity of the first, second Mack modes and streaks to steady wall-normal blowing/suction and wall heat flux. T…