Numerical Simulation of Supersonic Shear Layer with Plasma Actuator-Reference-Cited by-同舟云学术

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Numerical Simulation of Supersonic Shear Layer with Plasma Actuator

Published:2015 Issue: Volume:126 Page:44-48
ISSN:1877-7058
Container-title:Procedia Engineering
language:en
Short-container-title:Procedia Engineering

Author:

Lin Ke,Yan Hong

Publisher

Elsevier BV

Subject

Applied Mathematics

Reference6 articles.

1. Sound generation in a mixing layer;Lele;J. Fluid Mech.,1997

2. Orderly Structure in Jet Turbulence;Crow;J. Fluid Mech.,1971

3. Perturbed Free Shear Layers;Ho;Annu. Rev. Fluid Mech.,1984

4. Active control of highspeed and high Reynolds number jets using plasma actuators;Samimy;J. Fluid Mech,2007

5. Development and use of localized arc filament plasma actuators for high-speed flow control;Utkin;J. Phys. D.,2007

Cited by 4 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Mixing enhancement in a subsonic-supersonic shear layer with a cavity splitter plate;Aerospace Science and Technology;2020-07

2. Mathematical Model of the Process of the Plasma Atomizing of the Rod Electrode to Produce of Titanium Powder;2020 International Conference on Information Technology and Nanotechnology (ITNT);2020-05-26

3. Measurement of Flow Perturbation Spectra in Mach 4.5 Corner Separation Zone;AIAA Journal;2018-07

4. Corner Separation Zone Response to Plasma Actuation in the Hypersonic Boundary Layer over a Compression Ramp;48th AIAA Plasmadynamics and Lasers Conference;2017-06-02

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