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 …
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 …
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 …
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 …
cavity are conducted to investigate the effects of wall-normal steady blowing on the …
Suppression of cavity flow oscillations via three-dimensional steady blowing
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 …
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 …
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 …
interaction position, is numerically investigated, aiming to control the shock-wave/boundary …
Feature extraction of fields of fluid dynamics data using sparse convolutional autoencoder
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 …
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
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 …
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 …
rectangular cavity have been studied experimentally in a small-scale acoustic wind tunnel …