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Effect of High-Fidelity Ice-Accretion Simulations on Full-Scale Airfoil Performance

Author
BROEREN, Andy P1 ; BRAGG, Michael B1 ; ADDY, Harold E2 ; LEE, Sam3 ; MOENS, Frédéric4 ; GUFFOND, Didier5
[1] University of Illinois at Urbana―Champaign, Urbana, Illinois 61801, United States
[2] NASA John H. Glenn Research Center at Lewis Field, Cleveland, Ohio 44135, United States
[3] ASRC Aerospace Corporation, Cleveland, Ohio 44135, United States
[4] ONERA, 92190 Meudon, France
[5] ONERA, 92322 Châtillon, France
Source

Journal of aircraft. 2010, Vol 47, Num 1, pp 240-254, 15 p ; ref : 40 ref

CODEN
JAIRAM
ISSN
0021-8669
Scientific domain
Aeronautics astronautics; Mechanical engineering; Mechanics acoustics; Transportation
Publisher
American Institute of Aeronautics and Astronautics, Reston, VA
Publication country
United States
Document type
Article
Language
English
Keyword (fr)
Aile Avion Aérodynamique Aéronef Décrochage écoulement Essai soufflerie Essai sur modèle Essai vraie grandeur Etude expérimentale Forme géométrique Givrage Glace Performance
Keyword (en)
Wing Airplane Aerodynamics Aircraft Stall Wind tunnel test Model test Full scale mockup test Experimental study Geometrical shape Icing Ice Performance
Keyword (es)
Ala Avión Aerodinámica Aeronave Desprendimiento flujo Ensayo túnel aerodinámico Ensayo sobre modelo Prueba sobre modelo en escala natural Estudio experimental Forma geométrica Capa escarcha Hielo Rendimiento
Classification
Pascal
001 Exact sciences and technology / 001D Applied sciences / 001D15 Ground, air and sea transportation, marine construction / 001D15I Air transportation and traffic

Discipline
Building. Public works. Transport. Civil engineering
Origin
Inist-CNRS
Database
PASCAL
INIST identifier
22997242

Sauf mention contraire ci-dessus, le contenu de cette notice bibliographique peut être utilisé dans le cadre d’une licence CC BY 4.0 Inist-CNRS / Unless otherwise stated above, the content of this bibliographic record may be used under a CC BY 4.0 licence by Inist-CNRS / A menos que se haya señalado antes, el contenido de este registro bibliográfico puede ser utilizado al amparo de una licencia CC BY 4.0 Inist-CNRS

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