Dye visualisation of inclined and skewed synthetic jets in a cross flow

Aeronautical Journal

Volumn 109, Issue 1093, 2005, Pages 147-155

  Zhong, S ^a   Garcillan, L ^a   Wood, N J ^a  

^a UNIVERSITY OF MANCHESTER   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

ACTUATORS; FLOW CONTROL; MICROELECTROMECHANICAL DEVICES; ORIFICES; REYNOLDS NUMBER; VISUALIZATION;

CROSS-FLOW; MEMS; STROUHAL NUMBERS; SYNTHETIC JETS;

JETS;

EID: 17444380126     PISSN: 00019240     EISSN: None     Source Type: Journal    
DOI: 10.1017/S0001924000000658     Document Type: Article

References (13)

1. GAD-EL-HAK, M. Modern developments in flow control, Applied Mechanics Reviews, 1996, 49, (7), pp 365-379.
2. HO, C-M. and TAI, Y-C. Review: MEMS and its applications for flow control, J Fluid Engineering, 1996, 118, pp 437-446.
3. AMITAY, M., SMITH, B.L. and GLEZER, A. Aerodynamic flow control using synthetic jet technology, AIAA Paper 98-0208, 1998.
4. AMITAY, M., KINBENS, V., PAREKH, D. and GLEZER, A. The dynamics of flow reattachment over a thick airfoil controlled by synthetic jet actuators, AIAA Paper 99-1001, 1999.
5. CROOK, A., SADRI, A.M. and WOOD N.J. The development and implementation of synthetic jets for control of separated flow, AIAA Paper 99-3176, 1999.
6. SMITH, B.L. and GLEZER, A. The formation and evolution of synthetic jets, Physics of Fluids, 1998, 10, (9), pp 2281-2297.
7. GLEZER, A. and AMITAY, M. Synthetic jets, Ann Rev Fluid Mech, 2002, 34, pp 503-529.
8. CROOK, A. and WOOD, N.J. A parametric investigation of a synthetic jet in quiescent conditions, 9th International Symposium on Flow Visualisation, Edinburgh, 2000.
9. BARBEROPOULOS, A.A. and GARRY, K.P. The effect of skewing on the vorticity produced by an airjet vortex generator, Aeronaut J, March 1998,102, (1013), pp 171-177.
10. ZHONO, S., MULLET, F. and WOOD, N.J. The interaction of synthetic jets with a laminar boundary-layer, The 7th Triennial Symposium on Flow Control, Measurement and Visualisation, Paper 308, Sorrento, Italy, August 2003.
11. TANG, H. and ZHONG, S. 2D simulation of circular synthetic jets in quiescent conditions, RAeS Aerospace Aerodynamics Research Conference, London, UK, September 2004.
12. TANG, H. and ZHONG, S. Development of prediction models for synthetic jets in quiescent conditions using FLUENT, The 43rd Aerospace Sciences Meeting and Exhibit, AIAA-2005-0104, Reno, Nevada, USA, January 2005.
13. ZHONG, S., GARCILLAN, L., POKUSEVSKI, Z. and WOOD, N.J. A PIV study of the effects of shape and orientation of the orifices of synthetic jets in quiescent conditions, The 2nd AIAA Flow Control Conference, AIAA paper 2004-2213, Portland, Oregon, USA, June 2004.