504
B. Arizmendi et al.
49. M. Papadakis, G. Zumwalt, R. Elangonan, G. Freund Jr, M. Breer, L. Whitmer, An
experimental method for measuring water droplet impingement efficiency on two-and threedimensional bodies, in 24th Aerospace Sciences Meeting (1989)
50. M. Papadakis, K.E. Hung, G.T. Vu, H.W. Yeong, C.S. Bidwell, M.D. Breer, T.J. Bencic,
Experimental Investigation of Water Droplet Impingement on Airfoils, Finite Wings, and an
S-duct Engine Inlet (National Aeronautics and Space Administration, Glenn Research Center,
Cleveland Ohio, 2002)
51. Y. Cao, C. Ma, Q. Zhang, J. Sheridan, Numerical simulation of ice accretions on an aircraft
wing. Aerosp. Sci. Technol. 23(1), 296–304 (2012)
52. J. Tsao, A. Rothmayer, A mechanism for ice roughness formation on an airfoil leading edge,
contributing to glaze ice accretion, in 36th AIAA Aerospace Sciences Meeting and Exhibit
(1998), p. 485
53. G. Fortin, A. Ilinca, J.-L. Laforte, V. Brandi, New roughness computation method and
geometric accretion model for airfoil icing. J. Aircr. 41(1), 119–127 (2004)
54. R.Z. Blackmore, E.P. Lozowski, A theoretical spongy spray icing model with surficial
structure. Atmos. Res. 49(4), 267–288 (1998)
55. R.Z. Blackmore, L. Makkonen, E. Lozowski, A new model of spongy icing from first
principles. J. Geophys. Res. Atmos. 107(D21), AAC-9 (2002)
56. W. Kong, H. Liu, Development and theoretical analysis of an aircraft supercooled icing model.
J. Aircr. 51, 975–986 (2014)
57. I. Nomenclature, Further refinement of the LEWICE SLD model, in 44th AIAA Aerospace
Sciences Meeting and Exhibit (2006)
58. T. Hedde, D. Guffond, Onera three-dimensional icing model. AIAA J. 33(6), 1038–1045
(1995)
59. S. Nilamdeen, W. Habashi, M. Aube, G. Baruzzi, FENSAP-ICE: Modeling of water droplets
and ice crystals, in Proceedings of the 1st AIAA Atmospheric and Space Environments
Conference (2009)
60. G. Gori, M. Zocca, M. Garabelli, A. Guardone, G. Quaranta, PoliMIce: a simulation
framework for three-dimensional ice accretion. Appl. Math. Comput. 267, 96–107 (2015)
61. G. Mingione, M. Barocco, Flight in icing conditions summary, French DGAC (1997)
62. S.G. Pouryoussefi, M. Mirzaei, M.-M. Nazemi, M. Fouladi, A. Doostmahmoudi, Experimental study of ice accretion effects on aerodynamic performance of an NACA 23012 airfoil.
Chinese J. Aeronaut. 29(3), 585–595 (2016)
63. M.B. Bragg, Effects of ice accretion on aircraft aerodynamics (1998)
64. K. Rosen, M. Potash, Forty years of helicopter ice protection experience at Sikorsky aircraft.
J. American Helicopter Soc. 26(3), 5–19 (1981)
65. K. Korkan, E. Cross Jr, T. Miller, Performance degradation of a model helicopter rotor with a
generic ice shape. J. Aircr. 21(10), 823–830 (1984)
66. K.D. Korkan, L. Dadone, R.J. Shaw, Performance degradation of helicopter rotor in forward
flight due to ice. J. Aircr. 22(8), 713–718 (1985)
67. R.K. Jeck, Icing design envelopes (14 CFR parts 25 and 29, Appendix c) converted to a
distance-based format, Technical Report, Federal Aviation Administration Technical Center
Atlantic City New Jersey (2002)
68. F. Palacios, J. Alonso, K. Duraisamy, M. Colonno, J. Hicken, A. Aranake, A. Campos,
S. Copeland, T. Economon, A. Lonkar, et al., Stanford university unstructured (SU 2): An
open-source integrated computational environment for multi-physics simulation and design,
in 51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace
Exposition (2013), p. 287
69. H. Jasak, A. Jemcov, Z. Tukovic, et al., OpenFOAM: A C++ library for complex physics simulations, in International Workshop on Coupled Methods in Numerical Dynamics, vol. 1000
(IUC Dubrovnik, Croatia, 2007), pp. 1–20
70. W.B. Wright, Users manual for the improved NASA Lewis ice accretion code LEWICE 1.6
(1995)
71. T. Cebeci, Calculation of flow over iced airfoils. AIAA J. 27(7), 853–861 (1989)
B. Arizmendi et al.
49. M. Papadakis, G. Zumwalt, R. Elangonan, G. Freund Jr, M. Breer, L. Whitmer, An
experimental method for measuring water droplet impingement efficiency on two-and threedimensional bodies, in 24th Aerospace Sciences Meeting (1989)
50. M. Papadakis, K.E. Hung, G.T. Vu, H.W. Yeong, C.S. Bidwell, M.D. Breer, T.J. Bencic,
Experimental Investigation of Water Droplet Impingement on Airfoils, Finite Wings, and an
S-duct Engine Inlet (National Aeronautics and Space Administration, Glenn Research Center,
Cleveland Ohio, 2002)
51. Y. Cao, C. Ma, Q. Zhang, J. Sheridan, Numerical simulation of ice accretions on an aircraft
wing. Aerosp. Sci. Technol. 23(1), 296–304 (2012)
52. J. Tsao, A. Rothmayer, A mechanism for ice roughness formation on an airfoil leading edge,
contributing to glaze ice accretion, in 36th AIAA Aerospace Sciences Meeting and Exhibit
(1998), p. 485
53. G. Fortin, A. Ilinca, J.-L. Laforte, V. Brandi, New roughness computation method and
geometric accretion model for airfoil icing. J. Aircr. 41(1), 119–127 (2004)
54. R.Z. Blackmore, E.P. Lozowski, A theoretical spongy spray icing model with surficial
structure. Atmos. Res. 49(4), 267–288 (1998)
55. R.Z. Blackmore, L. Makkonen, E. Lozowski, A new model of spongy icing from first
principles. J. Geophys. Res. Atmos. 107(D21), AAC-9 (2002)
56. W. Kong, H. Liu, Development and theoretical analysis of an aircraft supercooled icing model.
J. Aircr. 51, 975–986 (2014)
57. I. Nomenclature, Further refinement of the LEWICE SLD model, in 44th AIAA Aerospace
Sciences Meeting and Exhibit (2006)
58. T. Hedde, D. Guffond, Onera three-dimensional icing model. AIAA J. 33(6), 1038–1045
(1995)
59. S. Nilamdeen, W. Habashi, M. Aube, G. Baruzzi, FENSAP-ICE: Modeling of water droplets
and ice crystals, in Proceedings of the 1st AIAA Atmospheric and Space Environments
Conference (2009)
60. G. Gori, M. Zocca, M. Garabelli, A. Guardone, G. Quaranta, PoliMIce: a simulation
framework for three-dimensional ice accretion. Appl. Math. Comput. 267, 96–107 (2015)
61. G. Mingione, M. Barocco, Flight in icing conditions summary, French DGAC (1997)
62. S.G. Pouryoussefi, M. Mirzaei, M.-M. Nazemi, M. Fouladi, A. Doostmahmoudi, Experimental study of ice accretion effects on aerodynamic performance of an NACA 23012 airfoil.
Chinese J. Aeronaut. 29(3), 585–595 (2016)
63. M.B. Bragg, Effects of ice accretion on aircraft aerodynamics (1998)
64. K. Rosen, M. Potash, Forty years of helicopter ice protection experience at Sikorsky aircraft.
J. American Helicopter Soc. 26(3), 5–19 (1981)
65. K. Korkan, E. Cross Jr, T. Miller, Performance degradation of a model helicopter rotor with a
generic ice shape. J. Aircr. 21(10), 823–830 (1984)
66. K.D. Korkan, L. Dadone, R.J. Shaw, Performance degradation of helicopter rotor in forward
flight due to ice. J. Aircr. 22(8), 713–718 (1985)
67. R.K. Jeck, Icing design envelopes (14 CFR parts 25 and 29, Appendix c) converted to a
distance-based format, Technical Report, Federal Aviation Administration Technical Center
Atlantic City New Jersey (2002)
68. F. Palacios, J. Alonso, K. Duraisamy, M. Colonno, J. Hicken, A. Aranake, A. Campos,
S. Copeland, T. Economon, A. Lonkar, et al., Stanford university unstructured (SU 2): An
open-source integrated computational environment for multi-physics simulation and design,
in 51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace
Exposition (2013), p. 287
69. H. Jasak, A. Jemcov, Z. Tukovic, et al., OpenFOAM: A C++ library for complex physics simulations, in International Workshop on Coupled Methods in Numerical Dynamics, vol. 1000
(IUC Dubrovnik, Croatia, 2007), pp. 1–20
70. W.B. Wright, Users manual for the improved NASA Lewis ice accretion code LEWICE 1.6
(1995)
71. T. Cebeci, Calculation of flow over iced airfoils. AIAA J. 27(7), 853–861 (1989)