Suppressing unsteady motion of shock wave by high-frequency plasma synthetic jet-Reference-Cited by-同舟云学术

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Suppressing unsteady motion of shock wave by high-frequency plasma synthetic jet

Published:2021-09 Issue:9 Volume:34 Page:60-71
ISSN:1000-9361
Container-title:Chinese Journal of Aeronautics
language:en
Short-container-title:Chinese Journal of Aeronautics

Author:

LUO Yanhao,LI Jun,LIANG Hua,GUO Shanguang,TANG Mengxiao,WANG Hongyu

Funder

National Natural Science Foundation of China

National Key Research and Development Program of China

Publisher

Elsevier BV

Subject

Mechanical Engineering,Aerospace Engineering

Reference34 articles.

1. Shock unsteadiness creation and propagation: experimental analysis;Benay;Shock Waves,2012

2. Effect of a transverse plasma jet on a shock wave induced by a ramp;Wang;Chin J Aeronaut,2017

3. Flow control of micro-ramps on supersonic forward-facing step flow;Zhang;Chinese Phys B,2016

4. Estruch-Samper D, Vanstone L, Ganapathisubramani B, et al. Effect of roughness-induced disturbances on axisymmetric hypersonic laminar boundary layer. Reston: AIAA; 2013. Report No.: AIAA-2013-0083.

5. Numerical study of blowing and suction control mechanism on NACA0012 airfoil;Huang;J Aircr,2004

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1. Three-dimensional Flow Field Characteristics of a Normal Slot Plasma Synthetic Jet Actuator;Journal of Applied Fluid Mechanics;2024-07-01

2. Investigation of control effects of end-wall self-adaptive jet on three-dimensional corner separation of a highly loaded compressor cascade;Chinese Journal of Aeronautics;2024-06

3. Study on the evolution stages of the flow field induced by an alternating current sliding discharge plasma actuator in different actuation modes;Physics of Fluids;2024-06-01

4. Direct numerical simulation of shock wave/boundary layer interaction controlled by steady microjet in a compression ramp;Chinese Journal of Aeronautics;2024-06

5. Large eddy simulation study on drag reduction performance of array-based plasma synthetic jet actuators;Chinese Journal of Aeronautics;2024-06

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