Online DMD-based adaptive feedback control targets and suppresses the resonant tone from shear-layer vortices in a supersonic dual-stream jet while preserving mean flow features.
Adaptive separation control of a laminar boundary layer using online dynamic mode decomposition.Journal of Fluid Mechanics, 903:A21
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Real-Time Adaptive Feedback Control of a Supersonic Dual-Stream Jet
Online DMD-based adaptive feedback control targets and suppresses the resonant tone from shear-layer vortices in a supersonic dual-stream jet while preserving mean flow features.