Erratum: Aerodynamics of scaled runback ice accretions (Journal of Aircraft (2008) 45:2 (591-603))

Journal of Aircraft

Volumn 45, Issue 3, 2008, Pages 1076-1088

  Whalen, Edward A ^a,b   Broeren, Andy P ^a,b   Bragg, Michael B ^a,b,c  

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

^b Department of Aerospace Engineering ^*

^c Research and Administrative Affairs

Author keywords

[No Author keywords available]

Indexed keywords

EID: 46449129941     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/1.38206     Document Type: Erratum

References (27)

1. Whalen, E. A., Broeren, A. P., Bragg, M. B., and Lee, S., "Characteristics of Runback Ice Accretions on Airfoils and Their Aerodynamic Effects," AIAA Paper 2005-1065, Jan. 2005.
2. Gray, V. H., and von Glahn, U. H., "Effect of Ice and Frost Formations on Drag of NACA 65B1B-212 Airfoil for Various Modes of Thermal Ice Protection," NACA TN-2962, June 1953.
3. Jacobs, E. N., "Airfoil Characteristics as Affected by Protuberances," NACA, Rept. 446, 1932.
4. 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.
5. Calay, R. K., Holdo, A. E., and Mayman, P., "Experimental Simulation of Runback Ice," Journal of Aircraft, Vol. 34, No. 2, March-April 1997, pp. 206-212.
6. Papadakis, M., and Gile-Laflin, B. E., "Aerodynamic Performance of a Tail Section with Simulated Ice Shapes and Roughness," AIAA Paper 2001-0539, Jan. 2001.
7. Lee, S., and Bragg, M. B., "Investigation of Factors Affecting Iced-Airfoil Aerodynamics," Journal of Aircraft, Vol. 40, No. 3, May-June 2003, pp. 499-508.
8. Broeren, A. P., and Bragg, M. B., "Effect of Airfoil Geometry on Performance with Simulated Intercycle Ice Accretions," Journal of Aircraft, Vol. 42, No. 1, Jan.-Feb. 2005, pp. 121-130.
9. Broeren, A. P., Lee, S., LaMarre, C. M., and Bragg, M. B., "Effect of Airfoil Geometry on Performance with Simulated Ice Accretions Volume 1: Experimental Investigation," Federal Aviation Administration, Washington, D.C., Office of Aviation Research DOT/FAA/AR-03/64, Aug. 2003.
10. Schofield, W. H., and Logan, E., "Turbulent Shear Flow over Surface Mounted Obstacles," Transactions of the ASME Journal of Fluids Engineering, Vol. 112, Dec. 1990, pp. 376-385.
11. Sullerey, R. K., Mishra, S., and Pradeep, A. M., "Application of Boundary Layer Fences and Vortex Generators in Improving Performance of S-Duct Diffusers," Transactions of the ASME Journal of Fluids Engineering, Vol. 124, No. 1, March 2002, pp. 136-142.
12. Lin, J. C., "Review of Research on Low-profile Vortex Generators to Control Boundary-Layer Separation," Progress in Aerospace Sciences, Vol. 38, Nos. 4-5, May/July 2002, pp. 389-420. doi:10.1016/S0376-0421(02)00010-6
13. Lee, S., "Effect of Supercooled Large Droplet Icing on Airfoil Aerodynamics," Ph.D. Dissertation, Department of Aeronautical and Astronautical Engineering, Univ. of Illinois, Urbana, IL, 2001.
14. Rae, W. H., and Pope, A., Low-Speed Wind Tunnel Testing, 2nd ed., Wiley, New York, 1984, pp. 349-362.
15. Kline, S. J., and McClintock, F. A., "Describing Uncertainties in Single-Sample Experiments," Mechanical Engineering, Vol. 75, No. 1, Jan. 1953, pp. 3-8.
16. Coleman, H. W., and Steele, W. G., Experimentation and Uncertainty Analysis for Engineers, Wiley, New York, 1989, pp. 40-118.
17. Federal Aviation Administration Pt. 25 (FAR 25), "Airworthiness Standards: Transport Category Airplanes, Appendix C," Washington, D.C., Department of Transportation, Federal Aviation Administration, 1974.
18. Braslow, A. L., and Knox, E. C., "Simplified Methods for Determination of Critical Height of Distributed Roughness Particles for Boundary-Layer Transition at Mach Numbers from 0 to 5," NACA TN-4363, Sept. 1958.
19. Drela, M., XFOIL Subsonic Airfoil Development System, http://raphael.mit.edu/xfoil/.
20. White, F. M., Viscous Fluid Flow, 2nd ed., McGraw-Hill, New York, 1991, pp. 242-247.
21. Coles, D., "The Law of the Wake in the Turbulent Boundary-Layer," Journal of Fluid Mechanics, Vol. 1, Pt. 2, July 1956, pp. 191-226. doi:10.1017/S0022112056000135
22. Whalen, E. A., Broeren, A. P., and Bragg, M. B., "Reynolds Number Considerations for Aerodynamic Testing of Simulated Runback Ice Accretions," AIAA Paper 2006-0260, Jan. 2006.
23. Gurbacki, H. M., and Bragg, M. B., "Unsteady Aerodynamic Measurements on an Iced Airfoil," AIAA Paper 2002-0241, Jan. 2002.
24. Addy, H. E., and Chung, J. J., "A Wind Tunnel Study of Icing Effects on a Natural Laminar Flow Airfoil," AIAA Paper 2000-0095, Jan. 2000.
25. Blumenthal, L. A., Busch, G. T., Broeren, A. P., and Bragg, M. B., "Issues in Ice Accretion Simulation on a Subscale Model," AIAA Paper 2006-0262, Jan. 2006.
26. McCullough, G. B., and Gault, D. E., "Examples of Three Representative Types of Airfoil-Section Stall at Low Speed," NACA TN-2502, Sept. 1951.
27. Morgan, H. L., Ferris, J. C., and McGhee, R. J., "A Study of High-Lift Airfoils at High Reynolds Numbers in the NASA Langley Low-Turbulence Pressure Tunnel," NASA TM-89125, 1987.