Characteristics of runback ice accretions on airfoils and their aerodynamic effects

43rd AIAA Aerospace Sciences Meeting and Exhibit - Meeting Papers

Volumn , Issue , 2005, Pages 207-220

  Whalen, Edward A ^a,c   Broeren, Andy P ^a,c,d   Bragg, Michael B ^a,c,d   Lee, Sam ^b,e  

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

^b QSS GROUP INC   (United States)

^c Department of Aerospace Engineering ^*  (United States)

^d AIAA   (United States)

^e NASA GLENN RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

DROPLET IMPINGEMENT; RESEARCH PROGRAM; THERMAL SYSTEMS;

AERODYNAMICS; DATA ACQUISITION; FLIGHT DYNAMICS; ICE; PHOTOGRAPHY; THERMOCOUPLES;

AIRFOILS;

EID: 30744431684     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (17)

1. 1-212 Airfoil for Various Modes of Thermal Ice Protection," NACA TN-2962, June, 1953.
2. Al-Kahlil, K.M., Miller, D., Wright, W., "Validation of Thermal Ice Protection Computer Codes: Part 3 - The Validation," AIAA 97-0051, Reno, NV, January, 1997.
3. Jacobs, E.N., "Airfoil Characteristics as Affected by Protuberances," NACA Report 446, 1932.
4. Lee, S. and Bragg, M.B., "Experimental Investigation of Simulated Large-Droplet Ice Shapes on Airfoil Aerodynamics," Journal of Aircraft, 36, 5, September-October 1999.
5. Calay, R.K., Holdo, A.E., Mayman, P., "Experimental Simulation of Runback Ice," Journal of Aircraft, 34, 2, March-April 1997.
6. Boeke, F.L. and Paselik, R.A., "Icing Problems and the Thermal Anti-Icing System," I.A.S. Meeting, Los Angeles, CA, August 16-17, 1945.
7. Wright, W.B., "User Manual for the NASA Lewis Ice Accretion Code LEWICE 2.0," NASA CR 209409, Jan. 1999.
8. Anderson, David N., "Manual of Scaling Methods," NASA CR 2004-212875, March 2004.
9. Drela, Mark, XFOIL Subsonic Airfoil Development System, http://raphael.mit.edu/xfoil/.
10. McCullough, G.B. and Gault, D.E., "Examples of Three Representative Types of Airfoil-Section Stall at Low Speed," NACA TN-2502, Washington, September 1951.
11. Lee, S., "Effect of Supercooled Large Droplet Icing on Airfoil Aerodynamics," Ph.D. Dissertation, Dept. of Aeronautical and Astronautical Eng., Univ. of Illinois, Urbana, IL, 2001.
12. Rae, W.H., and Pope, A., Low-Speed Wind Tunnel Testing, Wiley, New York, 1984, pp. 349-362.
13. Kline, S.J., and McClintock, F.A., "Describing Uncertainties in Single-Sample Experiments," Mechanical Engineering, Vol. 75, Jan. 1953, pp. 3-8.
14. Coleman, H.W., and Steele, W.G., Experimentation and Uncertainty Analysis for Engineers, John Wiley and Sons, New York, 1989, pp. 40-118.
15. Lee, S., and Bragg, M.B., "Experimental Investigation of Simulated Large-Droplet Ice Shapes on Airfoil Aerodynamics," Journal of Aircraft, Vol. 36, No. 5, Sept.-Oct. 1999, pp. 844-850.
16. Broeren, A.P. and Bragg, M.B., "Effect of Airfoil Geometry on Performance with Simulated Intercycle Ice Accretions," AIAA 2003-0728, Reno, NV, January, 2003.
17. Lee, S. and Bragg, M.B., "The Effect of Ridge-Ice Location and the Role of Airfoil Geometry," AIAA 20012481, Reno, NV, January, 2001.