Aeroacoustic investigation of transonic flow behavior in M219 deep cavity with passive flow control configurations

AE Şeker, B Zafer, I Gonzalez-Martino, M Yücetepe - Physics of Fluids, 2023 - pubs.aip.org
This study aims to investigate the effect of front and aft wall modifications and their
combinations on the sound pressure level response of the deep configuration of the M219 …

Hilbert–Huang spectral analysis of cavity flows incorporating fluidic spoilers

D Bacci, AJ Saddington - AIAA Journal, 2023 - arc.aiaa.org
Numerical aeroacoustic analysis was conducted on an M219 cavity geometry, incorporating
signature suppression features and leading-edge fluidic spoilers. The numerical model was …

Analysis of pressure fluctuation in transonic cavity flows using modal decomposition

H Liu, C Yan, Y Zhao, Y Qin - Aerospace Science and Technology, 2018 - Elsevier
Turbulent flows at a free stream Mach number of 1.19 over an open cavity with L/D ratio of
5.0 are numerically investigated using improved delayed detached-eddy simulation based …

Numerical analysis of transonic buffet flow around a hammerhead payload fairing

Y Liu, G Wang, H Zhu, Z Ye - Aerospace Science and Technology, 2019 - Elsevier
During ascent of launcher, the unsteady aerodynamic loads associated with transonic buffet
flow have become of considerable concern. To study the unsteady dynamics of buffet flow …

[HTML][HTML] Improved Delayed Detached-Eddy Investigations on the Flow Control of the Leading-Edge Flat Spoiler of the Cavity in the Low-Aspect-Ratio Aircraft

P Cui, G Zhou, Y Zhang, H Jia, X Wu, M Ma, H Li… - Aerospace, 2022 - mdpi.com
The internal weapon bay is widely used in modern aircraft; however, because the unsteady
flows of the cavity would cause dangerous store separation and intense aerodynamic noise …

Depth effects on the cavity induced transition at hypersonic speed by DNS

T Bai, Z Duan, Z Xiao - International Journal of Heat and Fluid Flow, 2022 - Elsevier
Cavity-induced transition (CIT) in a hypersonic boundary layer was simulated by employing
direct numerical simulation (DNS). The upwind Roe scheme was discretized by high-order …

Investigation of spectral characteristics by passive control methods past a supersonic cavity

K Luo, W Zhu, Z Xiao, Z Weng, L Deng, D Yang, J Liu - AIAA Journal, 2018 - arc.aiaa.org
Numerical investigations of the leading-edge sawtooth spoiler and slanted aft wall were
performed to explore the mechanisms of the suppression of pressure fluctuations in an open …

Simulations of transition and separation past a wind-turbine airfoil near stall

W Cui, Z Xiao, X Yuan - Energy, 2020 - Elsevier
The transition has an important effect on the aerodynamic performance and energy
consumption of the wind turbine. When the angle of attack is sufficiently large, separation …

Experimental research on reducing flow-induced cavity resonance with a narrowband active noise control system

F An, H Li, X Zhang, C Sun, B Liu - Applied Sciences, 2022 - mdpi.com
In this paper, active control of flow-induced cavity resonance noise is addressed. A hybrid
numerical method is presented to predict the resonance frequency and, instead of traditional …

Improvements for the DDES model with consideration of grid aspect ratio and coherent vortex structures

J Liu, J Chen, Z Xiao - Aerospace Science and Technology, 2024 - Elsevier
The delayed detached eddy simulation (DDES) model has achieved great success in
simulations of massive separations, but has been found to significantly delay the Kelvin …