Virtual aero-shaping of a Clark-Y airfoil using synthetic jet actuators

39th Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 2001, Pages

  Chatlynne, E ^a   Rumigny, N ^a   Amitay, M ^b   Glezer, A ^a  

^a GEORGIA INSTITUTE OF TECHNOLOGY   (United States)

^b GEORGIA TECH RESEARCH INSTITUTE   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMIC DRAG; AEROSPACE ENGINEERING; AIRFOILS; ANGLE OF ATTACK; FLOW SEPARATION; JETS; PRESSURE DISTRIBUTION; VELOCITY MEASUREMENT;

AERODYNAMIC SHAPE; ANGLES OF ATTACK; BASELINE CONFIGURATIONS; HIGH FREQUENCY HF; LIFTING SURFACES; PARTICLE IMAGE VELOCIMETRIES; RECIRCULATING FLOW; SYNTHETIC JET ACTUATORS;

ACTUATORS;

EID: 85088723152     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2001-732     Document Type: Conference Paper

References (14)

1. Seifert, A., Bachar, T., Koss, D., Shepshelovich, M. and I. Wygnanski, (1993). Oscillatory blowing: A tool to delay boundary-layer separation. A1AAJ. 37(11), 2052-2060.
2. th AIAA/NASA Aeroacoustics Conference, Williamsburg, VA.
3. Hsiao, F-B, Liu, C-F, and Shyu, J-Y (1990). Control of wall-separated flow by internal acoustic excitation. AIAA J. 28(8), 1440-1446.
4. Neuburger, D. and Wygnanski, I. The Use of a Vibrating Ribbon to Delay Separation on Two Dimensional Airfoils. TR-88-0004, 1987.
5. Williams, D., Acharya, M., Bernhardt, J., and Yang, P. The Mechanism of Flow Control on a Cylinder with the Unsteady Bleed Technique. AIAA Paper 91-0039, January 1991.
6. Chang, R.-C., Hsiao, F.-B., and Shyu, R.-N. Forcing Level Effects of Internal Acoustic Excitation on the Improvement of Airfoil Performance. Journal of Aircraft 29(5), 1992, pp. 823-829.
7. Smith, D. R., Amitay, M., Kibens, V., Parekh, D. E. and Glezer, A., Modification of Lifting Body Aerodynamics using Synthetic Jet Actuators, AIAA Paper 98-0209, January 1998.
8. Amitay, M., Kibens, V., Parekh, D. E. and Glezer, A., Flow Reattachment Dynamics over a Thick Airfoil Controlled by Synthetic Jet Actuators, AIAA Paper 99-1001, January 1999.
9. Amitay, M., Smith, D. R, Kibens, V., Parekh, D. E. and Glezer, A. Modification of the Aerodynamics Characteristics of an Unconventional Airfoil Using Synthetic Jet Actuators. Accepted for publication in the AIAA Journal, Vol. 39, No. 6, June 2001.
10. Erk, P. P. Separation Control on a Post-Stall Airfoil Using Acoustically Generated Perturbations. Ph.D. Dissertation, Technische Universitat Berlin, Germany, 1997.
11. Honohan, A.M, Amitay, M. and Glezer, A., Aerodynamic Control using Synthetic Jets, AIAA Paper 2000-2401, June 2000.
12. Perkins, C.D. and Hazen, D. Some recent advances in Boundary Layer and Circulation Control. Forth Anglo-American Aeronautical Conference, 1953.
13. Mandl, P. Effect of Standing Vortex on Flow about suction aerofoils with Split Flaps. Nat. Res. Council of Canada, Aero. Rep. No. 234, 1959.
14. Smith, B. L. and Glezer, A., The Formation and Evolution of Synthetic Jets, Physics of Fluids, Vol. 10, No. 9, 1998.