Resolvent-analysis-based design of airfoil separation control
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Publication:5235547
DOI10.1017/jfm.2019.163zbMath1430.76340arXiv1805.02128OpenAlexW2802019244MaRDI QIDQ5235547
Publication date: 14 October 2019
Published in: Journal of Fluid Mechanics (Search for Journal in Brave)
Full work available at URL: https://arxiv.org/abs/1805.02128
Boundary-layer theory, separation and reattachment, higher-order effects (76D10) General aerodynamics and subsonic flows (76G25) Flow control and optimization for incompressible viscous fluids (76D55)
Related Items (21)
On the origin of quadrupole sound from a two-dimensional aerofoil trailing edge ⋮ Transition, intermittency and phase interference effects in airfoil secondary tones and acoustic feedback loop ⋮ Identification and reconstruction of high-frequency fluctuations evolving on a low-frequency periodic limit cycle: application to turbulent cylinder flow ⋮ Sparsifying the resolvent forcing mode via gradient-based optimisation ⋮ Interpolatory input and output projections for flow control ⋮ Oblique transition in hypersonic double-wedge flow ⋮ Spike formation theory in three-dimensional flow separation ⋮ Mean resolvent operator of a statistically steady flow ⋮ An empirical model of noise sources in subsonic jets ⋮ Global stability analysis of elastic aircraft in edge-of-the-envelope flow ⋮ Resolvent-based optimal estimation of transitional and turbulent flows ⋮ Network broadcast analysis and control of turbulent flows ⋮ Resolvent-based estimation of space–time flow statistics ⋮ Resolvent-based study of compressibility effects on supersonic turbulent boundary layers ⋮ Resolvent analysis on the origin of two-dimensional transonic buffet ⋮ Cluster-based feedback control of turbulent post-stall separated flows ⋮ Optimal eddy viscosity for resolvent-based models of coherent structures in turbulent jets ⋮ Data-driven resolvent analysis ⋮ Efficient computation of global resolvent modes ⋮ A tale of two airfoils: resolvent-based modelling of an oscillator versus an amplifier from an experimental mean ⋮ Reinforcement-learning-based actuator selection method for active flow control
Uses Software
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