Iced-airfoil aerodynamics

Progress in Aerospace Sciences

Volumn 41, Issue 5, 2005, Pages 323-362

  Bragg, M B ^a   Broeren, A P ^a   Blumenthal, L A ^a  

^a University of Illinois at Urbana Champaign   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACCIDENT PREVENTION; AIRCRAFT; AIRFOILS; ICE; SURFACE ROUGHNESS;

AIRFOIL AERODYNAMICS; ICING RESEARCH PROGRAM; LEWIS WORKSHOP; MACH NUMBER;

AERODYNAMICS;

EID: 25144454031     PISSN: 03760421     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.paerosci.2005.07.001     Document Type: Review

References (110)

1. Gray VH. Prediction of aerodynamic penalties caused by ice formations on various airfoils. NASA TN D-2166, 1964.
2. Brumby RE. Wing surface roughness - cause & effect. D.C. Flight Approach, Jan. 1979. p. 2-7.
3. F.T. Lynch, and A. Khodadoust Effects of ice accretions on aircraft aerodynamics Prog Aerospace Sci 37 2001 669 767
4. Carroll TC, McAvoy WH. Formation of ice on airplanes. Airway Age, September 1928. p.58-9.
5. Jacobs EN. Airfoil section characteristics as affected by protuberances. NACA Report No. 446, 1932.
6. Jones R, Williams DH. The effect of surface roughness of the characteristics of the aerofoils NACA 0012 and RAF 34. British ARC, R&M No. 1708, 1936.
7. Gulick BG. Effects of simulated ice formation on the aerodynamic characteristics of an airfoil. NACA Wr L-292, 1938.
8. C.L. Johnson Wing loading, icing and associated aspects of modern transport design J Aero Sci 8 2 1940 43 54
9. Icing Research Tunnel. Program from the ASME dedication as an International Historic Mechanical Engineering Landmark, May 20, 1987.
10. Gray VH, Von Glahn UH. Effect of ice and frost formations on drag of NACA 65-212 airfoil for various modes of thermal ice protection. NACA TN 2962, June 1953.
11. Von Glahn UH, Gray VH. Effect of ice formations on section drag of swept NACA 63A-009 airfoil with partial-span leading-edge slat for various modes of thermal ice protection. NACA RM E53J30, March 15, 1954.
12. Bowden DT. Effect on pneumatic De-icers and ice formations on aerodynamic characteristics of an airfoil. NACA TN 3564, February 1954.
13. Gray VH, Von Glahn UH. Effect of ice and frost formations on drag of NACA 65-212 airfoil for various modes of thermal ice protection. NACA TN 2962, June 1953.
14. Gray VH, Von Glahn UH. Aerodynamic effects caused by icing of an unswept NACA 65A004 airfoil. NACA TN 4155, 1957.
15. Gray VH. Correlations among ice measurements, impingement rates, icing conditions, and drag coefficients for unswept NACA 65A004 airfoil. NACA TN 4151, February 1958.
16. Gray VH. Prediction of aerodynamic penalties caused by ice formations on various airfoils. NASA TN D-2166, 1964.
17. Aircraft Icing. Advisory group for aerospace research and development, Advisory Report No. 127, November 1978.
18. Ingelman-Sundberg M, Trunov OK, Ivaniko A. Methods for prediction of the influence of ice on aircraft flying characteristics. A Joint Report from the Swedish-Soviet Working Group on Flight Safety, Report No. JR-1, Board of Civil Aviation, Flight Safety Department, Norrkoping, Sweden, 1977.
19. Aircraft Icing. NASA Conference Publication 2086 or FAA-RD-78-109, July, 1978.
20. Potapczuk MG, Gerhart PM. Progress in the development of a Navier-Stokes solver for evaluation of iced airfoil performance. AIAA Paper 85-0410, 1985.
21. Cebeci T. Effects of environmentally imposed roughness on airfoil performance. NASA CR 179639, June, 1987.
22. Kwon O, Sankar L. Numerical study of the effects of ICING on finite wing aerodynamics. AIAA Paper 90-0757, 1990.
23. K.B.M.Q. Zaman, and M.G. Potapczuk The low frequency oscillation in the flow over a NACA airfoil with an iced leading edge T.J. Mueller Low reynolds number aerodynamics 1989 Springer New York 271 282
24. Bragg MB. Rime ice accretion and its effect on airfoil performance. Ph.D. Dissertation, The Ohio State University, 1981
25. and NASA CR 165599, 1982.
26. Flemming RJ, Lednicer DA. High speed ice accretion on rotorcraft airfoils. NASA CR 3910, 1985.
27. Bragg MB, Coirier WJ. Detailed measurements of the flow field in the vicinity of and airfoil with simulated glaze ice. AIAA Paper 86-0484, 1986.
28. M.B. Bragg, A. Khodadoust, and S.A. Spring Measurements in a leading-edge separation bubble due to a simulated airfoil ice accretion AIAA J 30 6 1992 1462 1467
29. Potapczuk MG, Bragg MB, Kwon OJ, Sankar LN. Simulation of iced wing aerodynamics. 68th AGARD fluid dynamics panel specialist meeting, Toulouse, France, April 29-May 1, 1991. p. 7-1-7-15.
30. Bragg MB, Khodadoust A, Soltani R, Wells S, Kerho M. Effect of a simulated ice accretion on the aerodynamics of a swept wing. AIAA Paper No. 91-0442, 1991.
31. Kerho M, Bragg MB. Helium bubble visualization of the spanwise separation on a NACA 0012 with simulated ice shape. AIAA Paper 92-0413, 1992.
32. Bragg MB, Kerho MF, Khodadoust A. LDV flowfield measurements on a straight and swept wing with a simulated ice accretion. AIAA Paper 93-0300, 1993.
33. Bragg MB, Khodadoust A. Experimental measurements in a large separation bubble due to a simulated glaze ice shape. AIAA Paper 88-0116, 1988.
34. Zierten TA, Hill EG. Effects of wing simulated ground frost on aircraft performance. VKI Lecture Series, 1987.
35. Van Hengst J, Boer JN. The effect of hoar-frosted wings on the FOKKER 50 m Take-off characteristics. AGARD CP 496, 1991.
36. M.B. Bragg, D.C. Heinrich, W.O. Valarezo, and R.J. McGhee Effect of underwing frost on a transport aircraft airfoil at flight reynolds number AIAA J Aircr 31 6 1994 1372 1379
37. M.F. Kerho, and M.B. Bragg Airfoil boundary-layer development and transition with large leading-edge roughness AIAA J 35 1 1997 75 84
38. Ashenden R, Lindburg W, Marwitz J. Two-dimensional NACA 23012 airfoil performance degradation by super cooled cloud, drizzle and rain drop icing. AIAA Paper 96-0870, 1996.
39. R. Ashenden, W. Lindburg, J.D. Marwitz, and B. Hoxie Airfoil performance degradation by supercooled cloud drizzle and rain drop icing AIAA J Aircr 33 6 1996 1040 1046
40. Miller DR, Addy Jr HE, Ide RF. A study of large droplet ice accretions in the NASA-Lewis IRT at near-freezing conditions. AIAA Paper 96-0934, 1996.
41. Addy Jr HE, Miller DR, Ide RF. A study of large droplet ice accretion in the NASA Lewis IRT at near-freezing conditions; Part 2. NASA TM-107424, April 1997, Prepared for the international conference on aircraft inflight icing, FAA, Springfield, VA, 1996.
42. S. Lee, and M.B. Bragg Experimental investigation of simulated large-droplet ice shapes on airfoil aerodynamics AIAA J Aircr 36 5 1999 844 850
43. Lee S, Bragg MB. Effects of simulated-spanwise ice shapes on airfoils: experimental investigation. AIAA Paper 99-0092, 1999.
44. R.K. Calay, A.E. Holdo, P. Mayman, and I. Lun Experimental simulation of runback ice AIAA J Aircr 34 2 1997 206 212
45. Kim HS, Bragg MB. Effects of leading-edge ice accretion geometry on airfoil aerodynamics. AIAA Paper 99-3150, 1999.
46. Papadakis M, Alansatan S, Seltmann M. Experimental study of simulated ice shapes on a NACA 0011 airfoil. AIAA Paper 99-0096, 1999.
47. Papadakis M, Alansatan S, Wong S. Aerodynamic characteristics of a symmetric NACA section with simulated ice shapes. AIAA Paper 2000-0098, 2000.
48. Addy Jr HE, Potapczuk MG, Sheldon DW. Modern airfoil ice accretions. AIAA Paper 97-0174, 1997.
49. Addy Jr HE. Ice accretions and icing effects for modern airfoils. NASA TP-2000-210031 also DOT/FAA/AR-99/89, April 2000.
50. Addy Jr HE, Chung JJ. A wind tunnel study of icing effects on a natural laminar flow airfoil. AIAA Paper 2000-0095, 2000.
51. Addy Jr HE, Broeren AP, Zoeckler JG, Lee S. A wind tunnel study of icing effects on a business jet airfoil. AIAA Paper 2003-0727, also NASA TM-2003-212124, 2003.
52. Gile-Laflin BE, Papadakis M. Experimental investigation of simulated ice accretions on a natural laminar flow airfoil. AIAA Paper 2001-0088, 2001.
53. Jackson DG, Bragg MB. Aerodynamic performance of an NLF airfoil with simulated ice. AIAA Paper 99-0373, 1999.
54. Broeren AP, Addy Jr HE, Bragg MB. Effect of intercycle ice accretions on airfoil performance. AIAA Paper 2002-0240, 2002.
55. Haines, AB, Young, AD. Scale effects on aircraft and weapon aerodynamics. AGARDograph 1994. p. 323.
56. T.A. Dunn, E. Loth, and M.B. Bragg Computational investigation of simulated large-droplet ice shapes on airfoil aerodynamics AIAA J Aircr 36 5 1999 836 843
57. Bragg MB, Loth E. Effects of large-droplet ice accretion on airfoil and wing aerodynamics and control. FAA/DOT/AR-00/14, Apr. 2000.
58. Pan J, Loth E, Bragg MB. RANS simulations of airfoils with ice shapes. AIAA Paper 2003-0729, 2003.
59. Chung JJ, Addy Jr HE. A numerical evaluation of icing effects on a natural laminar flow airfoil. AIAA Paper 2000-0096, 2000.
60. W.B. Wright Validation methods and results for a two-dimensional ice accretion code AIAA J Aircr 36 5 1999 827 835
61. Gurbacki HM, Bragg MB. Unsteady aerodynamic measurements on an iced airfoil. AIAA Paper 2002-0241, 2002.
62. Ratvasky TP, Van Zante JF, Riley JT. NASA/FAA Tailplane icing program overview. AIAA Paper 99-0370, 1999.
63. Papadakis M, Alansatan S, Yeong HW. Aerodynamic performance of a T-tail with simulated ice accretions. AIAA Paper 2000-0363, 2000.
64. Papadakis M, Yeong HW, Chandrasekharan R, Hinson M, Ratvasky TP, Giriunas J. Experimental investigation of simulated ice accretions on a full-scale T-tail. AIAA Paper 2001-0090, 2001.
65. Papadakis M, Yeong HW, Chandrasekharan R, Hinson M, Ratvasky TP. Effects of roughness on the aerodynamic performance of a business jet tail. AIAA Paper 2002-0242, 2002.
66. Vargas M, Reshotko E. Parametric experimental study of the formation of glaze ice shapes on swept wings. AIAA Paper 99-0094, 1999, also NASA TM-1998-206616.
67. Potapczuk MG, Papadakis M, Vargas M. LEWICE modeling of swept wing ice accretions. AIAA Paper 2003-0730, 2003.
68. Papadakis M, Yeong HW, Wong SC, Vargas M, Potapczuk MG. Aerodynamic performance of a swept wing with ice accretions. AIAA Paper 2003-0731, 2003.
69. Shin J. Characteristics of surface roughness associated with leading edge ice accretion. AIAA Paper 94-0799, 1994.
70. Anderson DN, Shin J. Characterization of ice roughness from simulated icing encounters. AIAA Paper 97-0052, 1997.
71. Kerho MF. Effect of large distributed roughness near an airfoil leading edge on boundary-layer development and transition. Ph.D. dissertation. Department of Aeronautical and Astronautical Engineering, University of Illinois, Urbana, IL, 1995.
72. Cummings MJ. Airfoil boundary-layer transition due to large isolated 3-D roughness elements in a favorable pressure gradient. M.S. Thesis, Department of Aeronautical and Astronautical Engineering, University of Illinois, Urbana, IL, 1995.
73. M.J. Cummings, and M.B. Bragg Boundary-layer transition due to isolated 3-D roughness on an airfoil leading edge AIAA J 34 9 1996 1949 1952
74. Bragg MB. Predicting airfoil performance with rime and glazed ice accretion. AIAA Paper 84-0106, 1984.
75. Cebeci T. The calculation of flow over iced airfoils. AIAA Paper 88-0112; 1988.
76. Jackson DG. Effect of simulated ice and residual ice roughness on the performance of a natural laminar flow airfoil. M.S. thesis, Department of Aeronautical and Astronautical Engineering, University of Illinois, Urbana, IL, 1999.
77. S. Lee, and M.B. Bragg Investigation of factors affecting iced-aircraft aerodynamics AIAA J Airc 40 3 2003 499 508
78. Bragg MB, Gregorek GM. Environmentally induced surface roughness effects on laminar flow airfoils: implications for flight safety. AIAA Paper 89-2049, 1989.
79. I. Tani Low speed flows involving bubble separations Prog Aero Sci 1964 70 103
80. W.B. Roberts Calculation of laminar separation bubbles and their effect on airfoil performance AIAA J 18 1 1980 25 31
81. Broeren AP, Addy HE, Bragg MB. Flowfield measurements about an airfoil with leading-edge ice shapes. AIAA Paper 2004-0059, 2004.
82. Khodadoust A. An experimental study of the flowfield on semispan rectangular wing with a simulated glaze ice accretion. Ph.D. Dissertation, Department of Aeronautical and Astronautical Engineering, University of Illinois, Urbana, IL, 1992.
83. Eaton JK, Johnston JP. A review of research on subsonic turbulent flow reattachment. AIAA J 1981;19(9): 1093-1100.
84. Gurbacki HM. Ice-induced unsteady flowfield effects on airfoil performance. Ph.D. Dissertation, Department of Aeronautical and Astronautical Engineering, University of Illinois, Urbana, IL, 2003.
85. A.P. Broeren, and M.B. Bragg Spanwise variation in the unsteady stalling flowfields of two-dimensional airfoil models AIAA J 39 9 2001 1641 1651
86. Broeren AP. An experimental study of unsteady flow over airfoils near stall. Ph.D. dissertation, Department of Mechanical and Industrial Engineering, University of Illinois, Urbana, IL, 2000.
87. Broeren AP, Bragg MB. Unsteady stalling characteristics of thin airfoils at low-Reynolds number, fixed and flapping wing aerodynamics for micro air vehicle applications. In: Mueller TJ, editor. Progress in astronautics and aeronautics, vol. 195; 2001. p. 191-213.
88. Driver DM, Seegmiller HL, Marvin JG. Unsteady behavior of a reattaching shear layer. AIAA Paper 83-1712, 1983.
89. D.M. Driver, H.L. Seegmiller, and J.G. Marvin Time-dependent behavior of a reattaching shear layer AIAA J 25 7 1987 914 919
90. M. Kiya, and K. Sasaki Structure of large-scale vortices and unsteady reverse flow in a reattaching zone of a turbulent separation bubble J Fluid Mech 154 1985 463 491
91. N.J. Cherry, R. Hillier, and M.E.M.P. Latour Unsteady measurements in a separated and reattaching flow J Fluid Mech 137 1983 83 113
92. D.G. Mabey Analysis and correlation of data on pressure fluctuations in separated flow AIAA J Aircr 9 1972 642 645
93. Hudy LM, Naguib AM, Humphreys WM, Bartram SM. Wall-pressure array measurements beneath a separated/reattaching flow region. AIAA Paper 2002-0597, 2002.
94. Papadakis M, Gile-Laflin BE. Aerodynamic performance of a tail section with simulated ice shapes and roughness. AIAA Paper 2001-0539, 2001.
95. Papadakis M, Gile-Laflin BE, Youssef GM, Ratvasky TP. Aerodynamic scaling experiments with simulated ice accretions. AIAA Paper 2001-0833, 2001.
96. Kim H. Effects of leading-edge ice accretion geometry on airfoil performance. MS thesis, Department of Aerospace Engineering, University of Illinois, Urbana, IL, 2004.
97. Olsen W, Shaw R, Newton J. Ice shapes and the resulting drag increase for a NACA 0012 airfoil. NASA TM-83556; 1983.
98. Bragg MB, Khodadoust A. Experimental measurements in a large separation bubble due to a simulated glaze ice shape. AIAA Paper 88-0116, 1988.
99. Blumenthal, LA. Surface pressure measurement on a three-dimensional ice shape. MS thesis, Department of Aerospace Engineering, University of Illinois, Urbana, IL, 2005.
100. Bragg MB, Gregorek GM. Aerodynamic characteristics of airfoils with ice accretions. AIAA Paper 82-0282, 1982.
101. Broeren AP, Addy HE, Bragg MB. Flowfield measurements about an airfoil with leading-edge ice shapes. AIAA Paper 2004-0059, 2004.
102. Bragg MB, Gregorek GM. Wind tunnel investigation of airfoil performance degradation due to icing. AIAA Paper 82-0582, 1982.
103. Lee S. Effects of supercooled large-droplet icing on airfoil aerodynamics. Ph.D. dissertation, Department of Aeronautical and Astronautical Engineering, University of Illinois, Urbana, IL, 2001.
104. Lee S, Dunn T, Gurbacki H, Bragg MB, Loth E. An experimental and computational investigation of spanwise-step-ice shapes on airfoil aerodynamics. AIAA Paper 98-0490, 1998.
105. Gurbacki H. Private communications. University of Illinois at Urbana-Champaign, Urbana, IL, April 2003.
106. Lee S, Kim HS, Bragg MB. Investigation of factors that influence iced-airfoil aerodynamics. AIAA Paper 2000-0099, 2000.
107. I.H. Abbott, and A.E. von Doenhoff Theory of wing sections 1959 Dover New York
108. S.F. Hoerner Fluid-dynamic lift 1975 Hoerner Fluid Dynamics Brick Town, NJ p. 4-19
109. Morgan HL, Ferris JC, McGhee RJ. A study of high-lift airfoils at high reynolds numbers in the langley low-turbulence pressure tunnel. NASA TM-89125, 1987.
110. Loftin Jr FT, Bursnall WJ. The effects of variations in reynolds number between 3.0 million and 25.0 million upon the aerodynamic characteristics of a number of NACA 6-series airfoil sections. NACA Report 964, 1950.