Use of piezoelectric actuators for airfoil separation control

AIAA Journal

Volumn 36, Issue 8, 1998, Pages 1535-1537

  Seifert, A ^a,b,c,d   Eliahu, S ^a,b   Greenblatt, D ^a,b   Wygnanski, I ^a,b,d  

^a TEL AVIV UNIVERSITY   (Israel)

^b Dept Fluid Mechanics Heat Transf ^*  (Israel)

^c NASA LANGLEY RESEARCH CENTER   (United States)

^d AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 0000244672     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.549     Document Type: Article

References (4)

1. Seifen, A., Darabi, A., and Wygnanski, I., "On the Delay of Airfoil Stall by Periodic Excitation," Journal of Aircraft, Vol. 33, No. 4, 1996, pp. 691-699.
2. Seifert, A., and Pack, L. G., "Oscillatory Control of Separation at High Reynolds Numbers," AIAA Paper 0214-98, Jan. 1998; also AIAA Journal (submitted for publication).
3. Rae, W. H., Jr., and Pope, A., Low Speed Wind Tunnel Testing, 2nd ed., Wiley, New York, 1984, pp. 349-361.
4. Lin, J. C., Selby, G. V., and Howard, F. G., "Exploratory Study of Vortex-Generating Devices for Turbulent Flow Separation Control," AIAA Paper 91-0042, Jan. 1991.