Experimental investigation of pitching and plunging airfoils at reynolds number between 1×104 and 6×104

Collection of Technical Papers - AIAA Applied Aerodynamics Conference

Volumn , Issue , 2009, Pages

  Baik, Yeon Sik ^a   Rauschy, Jonathan M ^a   Bernal, Luis P ^a   Ol, Michael V ^b,c  

^a UNIVERSITY OF MICHIGAN   (United States)

^b AIR FORCE RESEARCH LABORATORY   (United States)

^c WRIGHT PATTERSON AIR FORCE BASE   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; FLOW FIELDS; FLOW SEPARATION; REYNOLDS NUMBER; VELOCITY MEASUREMENT;

EXPERIMENTAL INVESTIGATIONS; FLOW TRANSITIONS; LAMINAR TO TURBULENT TRANSITIONS; PARTICLE IMAGE VELOCIMETRY TECHNIQUE; PIV MEASUREMENTS; SEPARATION CHARACTERISTICS; TURBULENCE STATISTICS; UNIVERSITY OF MICHIGAN;

AIRFOILS;

EID: 85067321139     PISSN: 10485953     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2009-4030     Document Type: Conference Paper

References (6)

1. Shyy, W., Lian, Y., Tang, J., Viieru, D., and Liu, H., AErodynamics of Low Reynolds Number Flyers, Cambridge University Press, 2008.
2. Ol, M. V., Bernal, L. P., Kang, C., and Shyy, W., "Shallow and deep dynamic stall for flapping low Reynolds number airfoils," Experiments in Fluids, Vol.46, No.5, 2009, pp. 883-901.
3. McCroskey, W., Carr, L., and McAlister, K., "Dynamic Stall Experiments on Oscillating Airfoils," AIAA J., Vol.14, No.1, 1976, pp. 57-63.
4. 4," 27th AIAA Applied Aerodynamics Conference, AIAA-2009-4100, San Antonio, TX, 2009.
5. Ol, M. V., McAuliffe, B. R., Hanff, E. S., Scholz, U., and Kaehler, C., "Comparison of Laminar Separation Bubble Measurements on a Low Reynolds Number Airfoil in Three Facilities," 35th AIAA Fluid Dynamics Conference and Exhibit, AIAA-2005-5149, Toronto, ON, 2005.
6. 4," 47th AIAA Aerospace Sciences Meeting and Exhibit, AIAA-2009-2536, Orlando, FL, 2009.