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SIMULATION OF AIRCRAFT CONDENSATION TRAILS AND WAKE VORTICES INTERACTION

A technique of calculation of aircraft condensation trails (contrails) and wake vortices interaction is described. The technique is based on a suitable for real-time applications mathematical model of far wake utilizes the method of discrete vortices. The technique is supplemented by account of the...

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Principais autores: T. O. Aubakirov, V. T. Dedesh, A. I. Zhelannikov, A. N. Zamyatin
Formato: Artigo
Idioma:Russo
Publicado: Moscow State Technical University of Civil Aviation 2016-11-01
Series:Научный вестник МГТУ ГА
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Acceso en liña:https://avia.mstuca.ru/jour/article/view/118
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