Boundary-layer transition due to isolated three-dimensional roughness on airfoil leading edge

AIAA Journal

Volumn 34, Issue 9, 1996, Pages 1949-1952

  Cummings, M J ^a,b   Bragg, M B ^a,b  

^a UNIVERSITY OF ILLINOIS AT URBANA CHAMPAIGN   (United States)

^b AIAA ^*

Author keywords

[No Author keywords available]

Indexed keywords

AEROFOILS; BOUNDARY LAYERS; ICE; ROUGHNESS;

EID: 0030450188     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/3.13333     Document Type: Article

References (11)

1. Klebanoff, P. S., Schubauer, G. B., and Tidstrom, K. D., "Measurements of the Effect of Two-Dimensional and Three-Dimensional Roughness Elements on Boundary-Layer Transition," Journal of the Aeronautical Sciences, Vol. 22, No. 11, 1955, pp. 803, 804.
2. Smith, A. M. O., and Clutter, D. W., "The Smallest Height of Roughness Capable of Affecting Boundary-Layer Transition," Journal of the Aerospace Sciences, Vol. 26, No. 4, 1959.
3. Tani, I., Komoda, H., and Konatsu, Y., "Boundary-Layer Transition by Isolated Roughness," Rept. 375, Aeronautical Research Inst., Univ. of Tokyo, Japan, Nov. 1962.
4. Braslow, A. L., Hicks, R. M., and Harris, R. V., "Use of Grit-Type Boundary-Layer-Transition Trips on Wind Tunnel Models," NASA TN D-3579, 1966.
5. Morkovin, M. V., "Bypass Transition to Turbulence and Research Desiderata," NASA CP-2386, May 1984, pp. 161-204.
6. Von Doenhoff, A. E., and Horton, E. A., "A Low-Speed Experimental Investigation of the Effect of a Sandpaper Type of Roughness on Boundary-Layer Transition," NACA Rept. 1349, 1956.
7. Peterson, J. B., and Horton, E. A., "An Investigation of the Effect of a Highly Favorable Pressure Gradient on Boundary-Layer Transition as Caused by Various Types of Roughness on a 10-Foot-Diameter Hemisphere at Subsonic Speeds," NASA MEMO 2-8-59L, 1959.
8. Cummings, M. J., "Airfoil Boundary-Layer Transition Due to Large Isolated 3-D Roughness Elements in a Favorable Pressure Gradient," M.S. Thesis, Univ. of Illinois at Urbana-Champaign, IL, 1995.
9. Bragg, M. B., Kerho, M. F., and Cummings, M. J., "Airfoil Boundary Layer Due to Large Leading-Edge Roughness," AIAA Paper 95-0536, Jan. 1995.
10. Shin, J., "Characteristics of Surface Roughness Associated with Leading Edge Ice Accretion," AIAA Paper 94-0799, Jan. 1994.
11. Tani, I., "Effect of Two-Dimensional and Isolated Roughness on Laminar Flow," Boundary Layer and Flow Control, edited by G. V. Lachmann, Vol. 2, Pergamon, Oxford, England, UK, 1961, pp. 637-656.