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TsAGI Science Journal

ISSN Print: 1948-2590
ISSN Online: 1948-2604

TsAGI Science Journal

DOI: 10.1615/TsAGISciJ.2015013629
pages 915-926

ESTIMATION OF AERODYNAMIC CHARACTERISTICS OF AIRCRAFT IN FLIGHT IN ICING CONDITIONS

Nadezhda Anatolievna Borisova
JSC "Tupolev," 17 Academician Tupolev Embankment, Moscow, 105005, Russia
Dmitrii Vladimirovich Goryachev
JSC "Tupolev," 17 Academician Tupolev Embankment, Moscow, 105005, Russia
Anatolii Borisovich Koscheev
JSC "Tupolev," 17 Academician Tupolev Embankment, Moscow, 105005, Russia

ABSTRACT

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.


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