Investigation into clustering of synthetic jet actuators for flow separation control applications

Aeronautical Journal

Volumn 109, Issue 1091, 2005, Pages 35-44

  Liddle, S C ^a   Wood, N J ^a  

^a UNIVERSITY OF MANCHESTER   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY LAYERS; CAVITATION; FLOW CONTROL; JETS; ORIFICES; REYNOLDS NUMBER; VORTEX FLOW; WIND TUNNELS;

LEADING EDGE; SYNTHETIC JET ACTUATORS (SJA); VORTEX GENERATORS; YAW-AERODYNAMICS;

ACTUATORS;

EID: 14944352382     PISSN: 00019240     EISSN: None     Source Type: Journal    
DOI: 10.1017/S0001924000000518     Document Type: Article

References (10)

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2. PACK, L.G., SCHAEFFLER, N.W., YAO, C.S. and SEIFERT, A. Active control of separation from the slat shoulder of a supercritical aerofoil, AIAA Paper, June 2002, pp 2002-3156.
3. WATSON, M., JAWORSKI, A. J. and WOOD, N.J. A study of synthetic jets from rectangular and dual-circular orifices, Aeronaut J, 107, (1073) July 2003, pp 427-434.
4. SMITH, D.R. Interaction of a synthetic jet with a crossflow boundary layer, AIM J, November 2002, 40, (11), pp 2277-2288.
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7. CROOK, A. PhD Thesis, 2002, University of Manchester, UK.
8. MORGAN, H.L., Experimental test results of the energy efficient transport (EET) flap-edge vortex model in the langley low-turbulence pressure tunnel, NASA TM-2002-211928, 2002.
9. LOCKERBY, D.A. and CARPENTER, P.W. Modeling and design of microjet actuators, AIAA J, February 2004, 42, (2), pp 220-227.
10. AMITAY, M. and GLEZER, A. Role of actuation frequency in controlled flow reattachment over a stalled aerofoil, AIAA J, 40, (2) February 2002, pp 209-216.