A wind tunnel study of icing effects on a business jet airfoil

41st Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 2003, Pages

  Addy Jr , Harold E ^a   Broeren, Andy P ^b   Zoeckler, Joseph G ^a   Lee, Sam ^c  

^a NASA GLENN RESEARCH CENTER   (United States)

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

^c QSS GROUP INC   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 84894699911     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (22)

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4. Addy, Jr., H. E. and Chung, J. J., "A Wind Tunnel Study of Icing Effects on a Natural Laminar Flow Airfoil, " AIAA Report No. 2000-0095, Jan., 2000.
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10. Reehorst, A. L. and Richter, G. P., "New Methods and Materials for Molding and Casting Ice Formations, " NASA TM No. 100126, September, 1987.
11. Vickerman, M., Choo, Y., Braun, D., Baez, M., and Gnepp, S. "SmaggIce: Surface Modeling and Grid Generation for Iced Airfoils-Phase 1 Results, " AIAA Report No. 2000-0235, January 2000.
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16. nd Ed., McGraw-Hill, New York, 1990, p. 279.
17. Wootton, L. R., "The Effect of Compressibility on the Maximum Lift Coefficient of Aerofoils at Subsonic Airspeeds, " Journal of the Royal Aeronautical Society, Vol. 71, July 1967, pp. 476-486.
18. Furlong, G. C., and Fitzpatrick, J. E., "Effects of Mach Number and Reynolds Number on the Maximum Lift Coefficient of a Wing of NACA 230-Series Airfoil Sections, " NACA TN-1299, May 1947.
19. 6 on the Maximum Lift Coefficient of a Wing of NACA 66-Series Airfoil Sections, " NACA TN-2251, Dec. 1950.
20. Morgan, H. L., Jr., Ferris, J. C., and McGhee, R. J., "A Study High-Lift Airfoils in the Langley Low-Turbulence Pressure Tunnel, " NASA TM 89125, July 1987.
21. Broeren, A. P., Addy, H. E., Jr., and Bragg, M. B., "Effect of Intercycle Ice Accretions on Airfoil Performance, " AIAA Paper 2002-0240, Jan. 2002.
22. Bragg, M. B., Khodadoust, A., and Spring, S. A., "Measurements in a Leading-Edge Separation Bubble due to a Simulated Airfoil Ice Accretion, " AIAA Journal, Vol. 30, No. 6, June, 1992, pp. 1462-1467.