年間 6 号発行
ISSN 印刷: 1948-2590
ISSN オンライン: 1948-2604
EFFECT OF ICING ON THE AERODYNAMIC CHARACTERISTICS OF AIRCRAFT DURING LANDING
要約
A methodology for the numerical investigation of the icing effect on the flow over a wing with a deflected slat and flap is presented. Meshes near the wing with and without icing are constructed using the original algorithm of swept volume mesh generation. The effects on the wing/fuselage aerodynamic characteristics are evaluated for various ice accretions as a result of the absence or malfunction of the anti-icing system. The numerical results are compared with the experimental data from the wind-tunnel tests of an aircraft model with artificial ice shapes.
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Mikhailovskiy K.V., Baranovski S.V., Accounting for Icing in the Design Analysis of Polymer Composite Wings, Proceedings of Higher Educational Institutions. Маchine Building, 3 (708), 2019. Crossref