空腔可压缩流致噪声问题研究进展

王显圣, 杨党国, 刘俊, 周方奇, 施傲 - 实验流体力学, 2018 - syltlx.com
空腔是一种常见的飞行器结构, 高速来流条件下, 空腔流致噪声成为重要噪声源,
制约飞行器性能的提高. 针对空腔可压缩流致噪声问题的研究进展进行综述 …

Excitation of free shear-layer instabilities for high-speed flow control

M Samimy, N Webb, M Crawley - AIAA journal, 2018 - arc.aiaa.org
Free shear layers are building blocks of many flows of interest in applications, including jets,
cavity flows, and separated flows. It was found several decades ago that free shear layers …

Control of cavity flow with acoustic radiation by an intermittently driven plasma actuator

H Yokoyama, K Otsuka, K Otake, M Nishikawara… - Physics of …, 2020 - pubs.aip.org
In a cavity flow with acoustic radiation, self-sustained oscillations are controlled by a
continuously or intermittently driven plasma actuator with elongated electrodes in the …

Coupling modes in supersonic twin rectangular jets

A Ghassemi Isfahani, NJ Webb, M Samimy - AIAA Scitech 2021 Forum, 2021 - arc.aiaa.org
View Video Presentation: https://doi. org/10.2514/6.2021-1292. vid In the closely spaced
twin-jet configuration often seen in military aircraft, the jets can become coupled, resulting in …

Reinventing the wheel: excitation of flow instabilities for active flow control using plasma actuators

M Samimy, N Webb, A Esfahani - Journal of Physics D: Applied …, 2019 - iopscience.iop.org
Flow control is typically used to manipulate a flow's natural behavior to alter its effects on a
vehicle or system. When active flow control (AFC) is used in aerospace applications, the …

Experimental investigation of the supersonic cavity by spectral-POD of high-sampling rate pressure-sensitive paint data

Y Oka, Y Ozawa, T Nagata, K Asai, T Nonomura - Experiments in Fluids, 2023 - Springer
A pressure distribution inside a two-dimensional rectangular cavity with a ratio L/D= 5.0 of
the cavity length L to the depth D over a supersonic flow was obtained using an improved …

Control of pressure oscillations induced by supersonic cavity flow

W Xiansheng, Y Dangguo, L Jun, Z Fangqi - AIAA Journal, 2020 - arc.aiaa.org
A control method is developed to suppress pressure oscillations induced by supersonic
cavity flow using high-speed upstream injection. The injection is generated with a large …

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 …

[图书][B] Energy deposition for high-speed flow control

D Knight - 2019 - books.google.com
Written by a leading expert in the field, this book presents a novel method for controlling high-
speed flows past aerodynamic shapes using energy deposition via direct current (DC), laser …

Characterization of three-electrode SparkJet actuator for hypersonic flow control

Y Zhou, Z Xia, Z Luo, L Wang, X Deng, Q Zhang… - AIAA Journal, 2019 - arc.aiaa.org
AERODYNAMIC control is one of the major challenges in supersonic/hypersonic vehicle
design. Effective manipulation of the flowfield can lead to a number of significant benefits to …