Publicou 6 edições por ano
ISSN Imprimir: 1948-2590
ISSN On-line: 1948-2604
COMPUTATION OF ICE SHAPES ON AN AIRFOIL
RESUMO
A procedure for the definition of trajectories and coefficients of overcooled droplets sinking on an airfoil was worked out and realized numerically for simulating the process of wing and helicopter blade icing. Similarity parameters of trajectories were specified. Computation of ice shapes on the airfoil NACA 00012 was fulfilled, and the obtained results were compared with known computational and experimental data.
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Trunov, O. K., Aircrafts Icing and Its Stoppers.
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Wright, W. Â., Gent, R. W., and Guffond, D., DRA/NASA/ONERA Collaboration on Icing Research, Part II. Prediction of Airfoil Ice Accretion.