Investigation of airfoil boundary layer and wake development at low Reynolds numbers

34th AIAA Fluid Dynamics Conference and Exhibit

Volumn , Issue , 2004, Pages

  Yarusevych, Serhiy ^a   Sullivan, Pierre E ^a   Kawall, John G ^b  

^a UNIVERSITY OF TORONTO   (Canada)

^b RYERSON UNIVERSITY   (Canada)

Author keywords

[No Author keywords available]

Indexed keywords

AIRFOILS; ANGLE OF ATTACK; REYNOLDS NUMBER; SEPARATION; WAKES; WIND TUNNELS;

BOUNDARY LAYER TRANSITIONS; BOUNDARY-LAYER SEPARATION; HOT WIRE ANEMOMETRY; LINEAR STABILITY THEORY; PERIODIC BOUNDARIES; SEPARATED SHEAR LAYERS; SURFACE PRESSURE MEASUREMENTS; WIND TUNNEL EXPERIMENT;

LAMINAR BOUNDARY LAYER;

EID: 85088344185     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2004-2551     Document Type: Conference Paper

References (15)

1. Lissaman, P. B. S., "Low-Reynolds-Number Airfoils," Annual Review of Fluid Mechanics, Vol. 15, 1982, pp. 223-239.
2. Mueller, T. J., and Batill, S. M., "Experimental Studies of Separation on a Two-Dimensional Airfoil at Low Reynolds Numbers," AIAA Journal, Vol. 20, No. 4, 1982, pp. 457-464.
3. Mueller, T. J., and DeLaurier, J. D., "Aerodynamics of Small Vehicles," Annual Review of Fluid Mechanics, Vol. 35, 2003, pp. 89-111.
4. Zaman, K. B. M. Q., "Effect of Acoustic Excitation on Stalled Flows over an Airfoil," AIAA Journal, Vol. 30, No. 6, 1992, pp. 1492-1499.
5. Yarusevych, S., Kawall, J. G., and Sullivan, P. E., "Effect of Acoustic Excitation on Airfoil Performance at Low Reynolds Numbers," AIAA Journal, Vol. 41, No. 8, 2003, pp. 1599-1601.
6. Haggmark, C. P., Bakchinov, P. H., and Alfredsson, P. H., "Measurements with a Flow Direction Boundary-Layer Probe in a Two-Dimensional Laminar Separation Bubble," Experiments in Fluids, Vol. 28, 2000, pp. 236-242.
7. Huang, R. F., and Lee, H. W., "Turbulence Effect on Frequency Characteristics of Unsteady Motions in Wake of Wing," AIAA Journal, Vol. 38,No. 1, 2000, pp. 87-94.
8. Lin, J. C. M., and Pauley, L. L., "Low-Reynolds-Number Separation on an Airfoil," AIAA Journal, Vol. 34, No. 8, 1996, pp.1570-1577.
9. Bullivant, W. K, "Test of the NACA 0025 and 0035 airfoils in the full-scale wind tunnel," NACA Report 708, 1941.
10. Brendel, M., and Mueller, T. J., "Boundary-Layer Measurements on an Airfoil at Low Reynolds Numbers," Journal of Aircraft, Vol. 25, No. 7, 1986, pp. 612-617.
11. Schlichting, H., and Gersten, K., Boundary layer theory, 8th ed., Springer-Verlag, New York, 2000, Chap. 15.
12. Kerho, M. F., and Bragg, M. B., "Airfoil Boundary Layer Development and Transition with Large Leading-Edge Roughness," AIAA Journal, Vol. 35, No. 1, 1997, pp. 75-84.
13. Dovgal, A. V., Kozlov, V. V., and Michalke, A., "Laminar Boundary Layer Separation: Instability and Associated Phenomena.," Prog. Aerospace Sci., Vol. 30, 1994, pp. 61-94.
14. Nishioka, M., Asai, M., and Yoshida, S., "Control of Flow Separation by Acoustic Excitation," AIAA Journal, Vol. 28, No.11, 1990, pp. 1909-1915.
15. Huang, R. F., and Lin, C. L., "Vortex Shedding and Shear-Layer Instability of Wing at Low-Reynolds Numbers," AIAA Journal, Vol. 33, No. 8, 1995, pp. 1398-1430.