Experimental study of ice accretion effects on aerodynamic performance of an NACA 23012 airfoil
Tóm tắt
Từ khóa
Tài liệu tham khảo
Venkataramani, 2007
Mason, 2007
Bragg, 2002
Ramezanizadeh, 2013, Experimental investigation on the ice accretion effects of airplane compressor cascade of stator blades on the aerodynamic coefficients, J Appl Fluid Mech, 6, 167
Potapczuk, 1991
Broeren, 2010, Aerodynamic simulation of runback ice accretion, J Aircraft, 47, 924, 10.2514/1.46475
Roberts, 1980, Calculation of laminar separation bubbles and their effect on airfoil performance, AIAA J, 18, 25, 10.2514/3.50726
Potapczuk MG, Bragg MB, Kwon OJ, Sankar LN. Simulation of iced wing aerodynamics. 68th AGARD Fluid Dynamic Specialist Meeting; Toulouse, France; 1991.
Bragg, 1992, Measurements in a leading-edge separation due to simulated airfoil ice accretion, AIAA J, 30, 1462, 10.2514/3.11087
Lee, 1999, Experimental investigation of simulated large droplet ice shapes on airfoil aerodynamics, J Aircraft, 36, 844, 10.2514/2.2518
Miller, 1996
Addy, 2000
Mirzaei, 2009, Numerical and experimental study of flow field characteristics of an iced airfoil, Aerosp Sci Technol, 13, 267, 10.1016/j.ast.2009.05.002
Diebold, 2013
Ansell, 2014, Characterization of low-frequency oscillations in the flowfield about an iced airfoil, AIAA J, 53, 629, 10.2514/1.J053206