Control of flow structure on a semi-circular planform wing

46th AIAA Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 2008, Pages

  Williams, D ^a   Collins, J ^a   Jankhot, C ^a   Colonius, T ^b   Tadmor, Gilead ^c  

^a ILLINOIS INSTITUTE OF TECHNOLOGY   (United States)

^b CALIFORNIA INSTITUTE OF TECHNOLOGY   (United States)

^c NORTHEASTERN UNIVERSITY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACTIVE FLOW CONTROL; DYNAMIC STALLS; FEEDBACK CONTROLLER; FLOW MODEL; FORCE BALANCE MEASUREMENTS; FREE-STREAM; LEADING EDGE; LIFT COEFFICIENT; OPEN LOOPS; PITCHING MOMENTS; PLANFORM; SMOKE-WIRE VISUALIZATION; SURFACE PRESSURE MEASUREMENTS; SURFACE PRESSURES; VORTEX LIFT;

AEROSPACE ENGINEERING; AIRFOILS; ASPECT RATIO; FEEDBACK CONTROL; LIFT DRAG RATIO; REYNOLDS NUMBER; VISUALIZATION;

PLANFORMS;

EID: 78049522075     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (5)

1. Birch, J.M., Dickson, W.B., Dickinson, M.H., "Force production and flow structure of the leading edge vortex on flapping wings at high and low Reynolds numbers, " J. of Experimental Biology, vol. 207, pp. 1063-1072.
2. Williams, D.R., Doshi, S., Collins, J., Colonius, T., "Control of the Spanwise Distribution of Circulation on NACA 0012 and Flat Plate Wings, " AIAA Paper 2007-1121.
3. st Conference on Active Flow Control, Berlin Germany, Sept. 27-29, 2006.
4. Dixon, C.J., "Lift Augmentation by Lateral Blowing Over a Lifting Surface, " AIAA Paper 69-193, AIAA/AHS VTOL Research, Design and Operations Meeting, Atlanta, GA, Feb. 1969.
5. Magill, J.C., Buchmann, M., Rixon, G., and McManus, K., "Dynamic Stall Control Using a Model-Based Observer, " J. Aircraft, Vol. 40, No. 2, 2003, pp. 355-362.