Flow Control of a NACA 0015 Airfoil Using a Chordwise Array of Synthetic Jets
Author:
Affiliation:
1. U.S. Air Force
2. Singapore Air Force
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2003-61
Reference13 articles.
1. Chen,F.J.,Yao,C.,Beeler,G.B.,Bryant,R.G., Fox,R.L."Development ofSyntheticJet Actuators forActiveFlowControl at NASALangley",AIAA 2000-2405,June2000
2. Honohan,A.M.,Amitay,M.,andGlezer,A. "AerodynamicControl usingSyntheticJets",AIAA 2000-2401,June2000
3. Hassan,A.A.,Munts,E.A."Transverseand Near-Tangent SyntheticJets forAerodynamicFlow Control",AIAA2000-4334,August 2000
4. Parekh, D.E., Glezer, A. "AVIA: Adaptive Virtual Aerosurface",AIAA2000-2474,June2000
5. Chatlynne, E., Rumigny, N., Amitay, M.,Glezer, A. "Virtual Aero-ShapingofaClark-YAirfoil UsingSyntheticJet Actuators",AIAA2001-0732, January2000
Cited by 2 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. Cavity Effect of Synthetic Jet Actuators Based on Piezoelectric Diaphragm;Applied Mechanics and Materials;2012-11
2. Collaborative Studies on Flow Separation Control;IUTAM Symposium on Flow Control and MEMS;2008
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