Modelling the noise emitted by turbulent jets is made difficult by their acoustic inefficiency:
only a tiny fraction of the near-field turbulent kinetic energy is propagated to the far field as …

This study is dedicated to achieving efficient active noise control in a supersonic
underexpanded planar jet, utilizing control parameters informed by resolvent analysis. The …

Trailing-edge (TE) noise is the main contributor to the acoustic signature of flows over
airfoils. It originates from the interaction of turbulent structures in the airfoil boundary layer …

Modes from global resolvent analyses have been shown to accurately model the
frequencies and spatial structure of the dominant coherent structures in several turbulent …