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

39th AIAA Fluid Dynamics Conference

Volumn , Issue , 2009, Pages

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

^a UNIVERSITY OF MICHIGAN   (United States)

^b AIR FORCE RESEARCH LABORATORY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

EXPERIMENTAL DATA; EXPERIMENTAL INVESTIGATIONS; FLAT PLATE; FLOW TOPOLOGY; FLOW TRANSITIONS; LEADING EDGE; PARTICLE IMAGE VELOCIMETRY TECHNIQUE; PHASE LAGS; PIV MEASUREMENTS; PLUNGING AIRFOIL; QUANTITATIVE ANALYSIS; SEPARATION CHARACTERISTICS; TRAILING EDGES; TURBULENCE STATISTICS; TURBULENT TRANSITION; UNIVERSITY OF MICHIGAN; WALL VELOCITY; WATER CHANNELS;

EXPERIMENTS; FLOW VISUALIZATION; FLUID DYNAMICS; REYNOLDS NUMBER; VELOCITY MEASUREMENT;

AIRFOILS;

EID: 77955926876     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     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., Bernai, 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-2009-536, Orlando, FL, 2009.