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.
Dynamic mode decomposition of numerical and experimental data.Journal of Fluid Mechanics, 656:5–28
1 Pith paper cite this work. Polarity classification is still indexing.
1
Pith paper citing it
fields
physics.flu-dyn 1years
2025 1verdicts
CONDITIONAL 1representative citing papers
citing papers explorer
-
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.