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FEATURES OF SPREAD OF VORTEX WAKE BEHIND AIRCRAFT AT TAKEOFF AND LANDING, IF CROSSWINDS

With cash-developed software system, were carried out research on the impact velocity crosswinds on the position of vortex wake at takeoff and landing of aircraft of various classes. Identify the threat, in terms of "hovering" of wing vortex over the center of the runway, crosswind speed. During tak...

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Hlavní autor: A. I. Zhelannikov
Médium: Artigo
Jazyk:Russo
Vydáno: Moscow State Technical University of Civil Aviation 2016-11-01
Edice:Научный вестник МГТУ ГА
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On-line přístup:https://avia.mstuca.ru/jour/article/view/245
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