Aerodynamic control at Low Angles of attack using trapped vorticity concentrations

Collection of Technical Papers - 44th AIAA Aerospace Sciences Meeting

Volumn 2, Issue , 2006, Pages 1258-1272

  DeSalvo, Michael E ^a   Glezer, Ari ^a  

^a GEORGIA INSTITUTE OF TECHNOLOGY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACTUATORS; ANGLE OF ATTACK; DRAG REDUCTION; PULSE MODULATION; VORTICITY; WAVEFORM ANALYSIS;

ACTUATION WAVEFORMS; UNSTABLE FREQUENCIES; VORTICITY CONCENTRATIONS;

WINGS;

EID: 34250741916     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2006-100     Document Type: Conference Paper

References (12)

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2. Glezer, A., Amitay, M., and Honohan, A. (2005) "Aspects of Low- and High-Frequency Actuation for Aerodynamic Flow Control," AIAA Journal 43(7), 1501-1511.
3. Smith, B. L. and Glezer, A. (1998). "The Formation and Evolution of Synthetic Jets," Physics of Fluids, Vol. 10, No. 9.
4. Glezer, A. and Amitay, M. (2002). "Synthetic Jets," Ann. Rev. Fluid Mech, 24.
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7. Amitay, M. and Glezer, A. (2002). "Controlled Transients of Flow Reattachment over Stalled Airfoils," International Journal of Heat Transfer and Fluid Flow, 23, 690-699.
8. Chatlynne, E., Rumigny, N., Amitay, M., and Glezer, A. (2001). "Virtual Aero-Shaping of a Clark-Y Airfoil using Synthetic Jet Actuators," AIAA Paper 2001-0732.
9. Amitay, M., Horvath, M., Michaux, M., and Glezer, A. (2001). "Virtual Aerodynamic Shape Modification at Low Angles of Attack using Synthetic Jet Actuators," AIAA Paper 2001-2975.
10. DeSalvo, M., Amitay, M., and Glezer, A. (2002). "Modification of the Aerodynamic Performance of Airfoils at Low Angles of Attack: Trailing Edge Trapped Vortices," AIAA Paper 2002-3165.
11. DeSalvo, M. and Glezer, A. (2004). "Aerodynamic Performance Modification at Low Angles of Attack by Trailing Edge Vortices," AIAA Paper 2004-2118.
12. DeSalvo, M. and Glezer, A. (2005). "Airfoil Aerodynamic Performance Modification using Hybrid Surface Actuators," AIAA Paper 2005-0872.