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

46th AIAA Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 2008, Pages

  Broeren, Andy P ^a   Bragg, Michael B ^a   Addy Jr , Harold E ^b   Lee, Sam ^c   Moens, Frédéric ^d   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)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMIC EFFECT; AERODYNAMIC EVALUATION; AERODYNAMIC PERFORMANCE; AERODYNAMIC SIMULATIONS; AIRFOIL AERODYNAMICS; AIRFOIL PERFORMANCE; CASTING SIMULATIONS; HIGH FIDELITY; ICE ACCRETION; ICE ACCRETION SIMULATION; ICE SIMULATION; LEADING EDGE; MAXIMUM LIFT COEFFICIENT; REYNOLDS; SIMULATION METHODS; SMALL VARIATIONS;

AEROSPACE ENGINEERING; COMPUTER SIMULATION; FLIGHT DYNAMICS; ICE; LIFT; MACH NUMBER; REYNOLDS NUMBER;

AIRFOILS;

EID: 78149456596     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

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