Effect of high-fidelity ice-accretion simulations on full-scale airfoil performance

Journal of Aircraft

Volumn 47, Issue 1, 2010, Pages 240-254

  Broeren, Andy P ^a,e   Bragg, Michael B ^a,e   Addy Jr , Harold E ^b,f   Lee, Sam ^c,g   Moens, Frédéric ^d,g   Guffond, Didier ^d  

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

^b NASA GLENN RESEARCH CENTER   (United States)

^c ASRC Aerospace Corp   (United States)

^d ONERA   (France)

^e Icing Branch

^f Applied Aerodynamics Department

^g Atmospheric Environment Research Unit

Author keywords

[No Author keywords available]

Indexed keywords

AIRFOILS; LIFT; MACH NUMBER; REYNOLDS NUMBER; WIND TUNNELS;

AERO-DYNAMIC PERFORMANCE; AERODYNAMIC EVALUATION; AERODYNAMIC SIMULATIONS; AIRFOIL AERODYNAMICS; CASTING SIMULATIONS; ICE ACCRETION SIMULATION; LOW REYNOLDS NUMBER; MAXIMUM LIFT COEFFICIENT;

ICE;

EID: 75749154458     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/1.45203     Document Type: Article

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