Investigation of factors that influence iced-airfoil aerodynamics

38th Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 2000, Pages

  Lee, Sam ^a   Kim, Han S ^a   Bragg, Michael B ^a  

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

Author keywords

[No Author keywords available]

Indexed keywords

EID: 51349087316     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (14)

1. Lee, S. and Bragg, M. B., "Effects of Simulated Spanwise-Ice Shapes on Airfoils: Experimental Investigation", AIAA Paper No. 99-0092, Reno, NV, January 11-14, 1999.
2. Kim, H.S. and Bragg, M.B., "Effects of Leading-Edge Ice Accretion Geometry on Airfoil Performance, " AIAA Paper
3. th Aerospace Sciences Meeting & Exhibit, Reno, NV 1998.
4. Rae, W. H. and Pope, A., Low-Speed Wind Tunnel Testing, John Wiley & Sons, 1984.
5. Shin, Jaiwon, and Bond, Thomas H., "Repeatability of Ice Shapes in the NASA Lewis Icing Research Tunnel", Journal of Aircraft, Vol. 3 1, No. 5, Sept-Oct. 1994.
6. Brumby, R.E., "Wing Surface Roughness-Cause & Effect, " D.C. Flight Approach, Jan. 1979, pp. 2-7.
7. Jacobs, E. N., "Airfoil Section Characteristics as Affected by Protuberances, " NACA Report No. 446, 1932.
8. Hoemer, S.F., Fluid-Dynamic Lift, Hoemer Fluid Dynamics, Brick Town, NJ, 1975, p4-19.
9. th Aerospace Sciences Meeting & Exhibit, Reno, NV 1999.
10. Gregory, N. and O'Reilly, C.L., "Low-Speed Aerodynamic Characteristics of NACA 0012 Aerofoil Section, including the Effects of Upper-Surface Roughness Simulating Hoar Frost, " ARC R&M 3726, Jan. 1970.
11. Bowden, D.T., "Effect of Pneumatic De-Icers and Ice Formations on Aerodynamic Character of an Airfoil, " NACA Technical Note 3564, February, 1956.
12. Abbott, I.H. and von Doenhoff, A.E., Theory of Wing Sections, Dover Publications, NY, 1959.
13. McGhee, R.J., Viken, J.K., Pfenninger, W., Beasley, W. D, and Harvey, W.D., "Experimental Results for a Flapped Natural-Laminar-Flow Airfoil with High Lift/Drag Ratio, " NASA TM 85788, May 1984.
14. Drela, M., "XFOIL 6.6 User Primer", MIT Aero & Astro Engineering, March 14, 1996.