Flow structures in flat plate boundary layer induced by pulsed plasma actuator
Author:
Publisher
Springer Science and Business Media LLC
Subject
General Engineering,General Materials Science
Link
http://link.springer.com/content/pdf/10.1007/s11431-010-4100-7.pdf
Reference38 articles.
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3. Zhang P F, Yan B, Wang J J. Novel circulation control method by plasma actuator. Technical Report, AIAA Paper 2010-5105. 2010
4. Zhang P F, Liu A B, Wang J J. Aerodynamic modification of a NACA 0012 airfoil by trailing-edge plasma Gurney flap. AIAA J, 2009, 47: 2467–2474
5. Corke T C, Jumper E J, Post M L, et al. Application of weakly-ionized plasmas as wing flow-control devices. Technical Re-port, AIAA Paper 2002-0350. 2002
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