TsAGI Science Journal
Publicado 6 números por año
ISSN Imprimir: 1948-2590
ISSN En Línea: 1948-2604
ESTIMATION OF AERODYNAMIC CHARACTERISTICS OF AIRCRAFT IN FLIGHT IN ICING CONDITIONS
Volumen 45,
Edición 8, 2014,
pp. 915-926
DOI: 10.1615/TsAGISciJ.2015013629
SINOPSIS
A description of a method used in the fast calculation of changes in the aircraft aerodynamic characteristics during flight under icing conditions is given in this paper. The presented dependences are based on the results of wind tunnel tests and flight tests of airplanes with ice simulators and under natural icing conditions. This method is most applicable at the initial stages of design.
PALABRAS CLAVE: method, icing, wing, aerodynamic characteristics, fast calculation,
flight tests, ice simulators, thickness of the ice
CITADO POR
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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
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