Shock and shear layer interactions in a confined supersonic cavity flow

SK Karthick - Physics of Fluids, 2021 - pubs.aip.org
The impinging shock of varying strengths on the free shear layer in a confined supersonic
cavity flow is studied numerically using the detached eddy simulation. The resulting …

Identity of attached eddies in turbulent channel flows with bidimensional empirical mode decomposition

C Cheng, W Li, A Lozano-Durán, H Liu - Journal of fluid mechanics, 2019 - cambridge.org
Bidimensional empirical mode decomposition (BEMD) is used to identify attached eddies in
turbulent channel flows and quantify their relationship with the mean skin-friction drag …

Metasurface zero-impedance matching mechanism for aerodynamic noise reduction

M Li, JH Wu, XY Yuan - Journal of Sound and Vibration, 2022 - Elsevier
In order to control the low-mid frequency aerodynamic noises, the zero-impedance matching
mechanism of a stepped multi-neck Helmholtz resonator (SMNHR) metasurface on a 1/4 …

Active control of pressure fluctuations in an incompressible turbulent cavity flow

JN Choi, JH Lee - Aerospace Science and Technology, 2023 - Elsevier
Large-eddy simulations of incompressible turbulent boundary layer flows over an open
cavity are conducted to investigate the effects of wall-normal steady blowing on the …

Suppression of cavity flow oscillations via three-dimensional steady blowing

Y Zhang, Y Sun, N Arora, LN Cattafesta III, K Taira… - AIAA journal, 2019 - arc.aiaa.org
This paper presents an investigation of the flow physics and control of cavity flow oscillations
using a three-dimensional (3-D) array of steady jets located near the cavity leading edge …

On the mechanism of acoustic resonances from a leading-edge slat

W Li, Y Guo, W Liu - Aerospace Science and Technology, 2021 - Elsevier
Implicit large-eddy simulations are performed to investigate the acoustic resonances from a
leading-edge slat at two different Reynolds numbers. Three types of acoustic waves are …

Large-eddy simulation of shock-wave/boundary-layer interaction control using a backward facing step

W Li, H Liu - Aerospace Science and Technology, 2019 - Elsevier
A new passive flow control method, putting a backward facing step ahead of the shock
interaction position, is numerically investigated, aiming to control the shock-wave/boundary …

Feature extraction of fields of fluid dynamics data using sparse convolutional autoencoder

W Obayashi, H Aono, T Tatsukawa, K Fujii - AIP Advances, 2021 - pubs.aip.org
A neural network technique that extracts underlying flow features from the original flow field
data is newly proposed. The technique here is based on the convolutional and sparse …

Effect of vortex and entropy sources in sound generation for compressible cavity flow

N Arya, A De - Physics of Fluids, 2021 - pubs.aip.org
The present study reports the effect of different source terms on the near and far-field
acoustic characteristics of compressible flow over a rectangular cavity using hybrid …

Experimental study on aerodynamic noise characteristics and control of non-fully open low-speed cavities

C Li, X Wang, Y Li - Applied Acoustics, 2023 - Elsevier
In this paper, the aerodynamic noise characteristics and control of a non-fully open
rectangular cavity have been studied experimentally in a small-scale acoustic wind tunnel …