Numerical Study for Active Flow Control Using Dielectric Barrier Discharge Actuators-Reference-Cited by-同舟云学术

Numerical Study for Active Flow Control Using Dielectric Barrier Discharge Actuators

Published:2017-09 Issue:5 Volume:30 Page:04017050
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Ji Shengcheng¹,Zhang Bei²,Li Jiang³,Wang Guangqiu⁴

Affiliation:

1. Senior Engineer, Dept. of Stress Analysis, Beijing Aeronautical Science and Technology Research Institute, Champing District, Beijing 102211, P.R. China (corresponding author).

2. Lecturer, Dept. of Measurement and Automation, School of Automation Science and Electrical Engineering, Beihang Univ., Xue Yuan Rd. No. 37, Haidian District, Beijing 100191, P.R. China.

3. Postdoc, Dept. of Strategic Research, Beijing Aeronautical Science and Technology Research Institute, Champing District, Beijing 102211, P.R. China.

4. Senior Researcher, Dept. of Strategic Research, Beijing Aeronautical Science and Technology Research Institute, Champing District, Beijing 102211, P.R. China.

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0000764

Reference25 articles.

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3. Benard N. Braud P. and Jolibois J. (2008). “Airflow reattachment along a NACA 0015 airfoil by surface SDBD actuator-time resolved PIV investigation.” 4th Flow Control Conf. Curran Associates Group Miami 4202.

4. Bouchmal A. (2011). “Modeling of dielectric-barrier discharge actuator-implementation validation and generalization of an electrostatic model.” M.Sc. thesis Delft Univ. of Technology Delft Netherlands.

5. Plasma flaps and slats: An application of weakly-ionized plasma actuators;Corke T. C.;J. Aircraft,2004

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