Effect of regular surface perturbations on flow over an airfoil

35th AIAA Fluid Dynamics Conference and Exhibit

Volumn , Issue , 2005, Pages

  Santhanakrishnan, Arvind ^a   Jacob, Jamey D ^a  

^a UNIVERSITY OF KENTUCKY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRFOILS; BOUNDARY LAYERS; SMOKE;

BOUNDARY-LAYER SEPARATION; FLUCTUATING VELOCITIES; PASSIVE FLOW CONTROL; QUALITATIVE OBSERVATIONS; REGULAR PERTURBATIONS; SURFACE PERTURBATIONS; TRANSITION TO TURBULENCE; VORTICAL STRUCTURES;

SHEAR FLOW;

EID: 85085402507     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2005-5145     Document Type: Conference Paper

References (24)

1. Mueller, T. and DeLaurier, J., "Aerodynamics of Small Vehicles, " Annual Rev. of Fluid Mech., Vol. 35, 2003, pp. 89-111.
2. Stanewsky, E., "Adaptive Wing and Flow Control Technology, " Progress in Aerospace Sciences, Vol. 37, 2001, pp. 583-667.
3. Lissaman, P., "Low-Reynolds-Number Airfoils, " Annual Rev. of Fluid Mech., Vol. 15, 1983, pp. 223-239.
4. Carmichael, B., "Low Reynolds Number Airfoil Survey, " NASA CR-165803, 1981.
5. Jacob, J., "On the Fluid Dynamics of Adaptive Airfoils, " Proc. ASME International Mechanical Engineering and Exposition, ASME, Anaheim, CA, 1998.
6. Gad-El-Hak, M., "Flow Control: The Future, " Journal of Aircraft, Vol. 38, 2001, pp. 402-418.
7. McMasters, J. and Henderson, M., "Low-Speed Single Element Airfoil Synthesis, " Technical Soaring, Vol. 6, 1980, pp. 1-21.
8. Gad-El-Hak, M., "Control of Low-Speed Airfoil Aerodynamics, " AIAA Journal, Vol. 28, 1990, pp. 1537-1552.
9. Jacobs, E., "Airfoil Section Characteristics as Affected by Protuberances, " NACA TR-446, 1932.
10. Jacobs, E., "Wing Characteristics as Affected by Protuberances of Short Span, " NACA TR-449, 1932.
11. Zaman, K. and Potapczuk, M., "The Low-Frequency Oscillation in the Flow Over a NACA 0012 Airfoil with an Iced Leading Edge, " Low Reynolds Number Aerodynamics, edited by T. Mueller, Springer-Verlag, New York, 1989, pp. 271-282.
12. Bragg, M. B., Cummings, M. J., and Henze, C. M., "Boundary-layer and heat-transfer measurements on an airfoil with simulated ice roughness, " AIAA Paper 1996-0866, 34th AIAA Aerospace Sciences Meeting, Reno, NV, Jan. 1996.
13. Lyon, C. A., Selig, M. S., and Broeren, A. P., "Boundary layer trips on airfoils at low Reynolds numbers, " AIAA Paper 1997-0511, 35th AIAA Aerospace Sciences Meeting, Reno, NV, Jan. 1997.
14. 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.
15. Usui, M., Simpson, A., Smith, S., and Jacob, J., "Development and Flight Testing of a UAV with Inflatable-Rigidizable Wings, " AIAA Paper 2004-1373, 42nd AIAA Aerospace Sciences Meeting, Reno, NV, Jan. 2004.
16. Huebsch, W., "Dynamic Surface Roughness for Aerodynamic Flow Control, " AIAA Paper 2004-0587, 42nd AIAA Aerospace Sciences Meeting, Reno, NV, Jan. 2004.
17. Miklosovic, D., Murray, M., Howle, L., and Fish, F., "Leading-Edge tubercules delay stall on humpback whale (Megaptera novaeangliae) flippers, " Phys. Fluids, Vol. 16, No. 5, May 2004, pp. 39-42.
18. Batill, S. and Mueller, T., "Visualization of Transition in the Flow Over an Airfoil Using the Smoke Wire Technique, " AIAA Journal, Vol. 19, 1981, pp. 340-345.
19. Sholl, M. and Savas, O., "A Fast Lagrangian PIV Method for Study of General High-Gradient Flows, " AIAA Paper 1997-0493, 35th AIAA Aerospace Sciences Meeting, Reno, NV, Jan. 1997.
20. Tsuei, L. and Savas, O., "Treatment of Interfaces in Particle Image Velocimetry, " Experiments in Fluids, Vol. 29, 1999, pp. 203-214.
21. Braslow, A., Hicks, R., and Harris, R., "Use of Grit-Type Boundary-Layer-Transition Trips on Wind Tunnel Models, " NASA TN D-3579, 1966.
22. OL, M. V., Hanff, E., McCauliffe, B., Scholz, U., and Kaehler, C., "Comparison of Low Reynolds Number Airfoil Laminar Separation Bubble Measurements in Three Facilities, " AIAA Paper 2005-5149, to be presented at the 35th AIAA Fluid Dynamics Conference and Exhibit, Toronto, Ontario, June 2005.
23. Yarusevych, S., Sullivan, P. E., and Kawall, J. G., "Investigation of Airfoil Boundary Layer and Wake Development at Low Reynolds Numbers, " AIAA Paper 2004-2551, 34th AIAA Fluid Dynamics Conference and Exhibit, Portland, Oregon, June 2004.
24. Schlichting, H. and Gersten, K., Boundary Layer Theory, Springer-Verlag, New York, 8th ed., 2000.