FEATURES OF SPREAD OF VORTEX WAKE BEHIND AIRCRAFT AT TAKEOFF AND LANDING, IF CROSSWINDS
Abstract
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 takeoff and landing aircraft, these vortices can be a danger to other aircraft.
References
1. Ginevskiyj A.S., Zhelannikov A.I. Vikhrevihe sledih samoletov [Vortex traces of planes]. Moscow. Fizmatlit, 2008, 170 p. (In Russian)
2. Aubakirov T.O., Zhelannikov A.I., Ivanov P.E., Nisht M.I. Sputnihe sledih i ikh vozdeyjst-vie na letateljnihe apparatih. Modelirovanie na EhVM [Wakes and their impact on aircraft. Modeling on the computer]. Almaty. 1999. 230 p. (In Russian)
3. Aubakirov T.O., Belocerkovskiyj S.M., Zhelannikov A.I., Nisht M.I. Nelineyjnaya teoriya krihla i ee prilozheniya [Non-linear wing theory and its applications]. Almaty. Gihlihm, 1997. 448 p. (In Russian)
4. Belocerkovskiyj S.M., Nisht M.I. Otrihvnoe i bezotrihvnoe obtekanie tonkikh krihljev idealjnoyj zhidkostjyu [Separated and unrepeated flow past thin wings of perfect fluid]. Moscow. Nauka, 1978. 277 p. (In Russian)
5. Belocerkovskiyj S.M., Ginevskiyj A.S. Modelirovanie turbulentnihkh struyj i sledov na osnove metoda diskretnihkh vikhreyj [Simulation of turbulent jets and traces based on the method of discrete vortices]. Moscow. Fizmatlit, 1995, 368 p. (In Russian)
6. Vihshinskiyj V.V., Sudakov G.G. Vikhrevoyj sled samoleta v turbulentnoyj atmosfere [Vortex trail of a plane in turbulent atmosphere. Proceedings of CAHI]. Moscow. Trudih CAGI, vihp. 2667, 2006, 155 p. (In Russian)
7. Aubakirov T.O., Dedesh V.T., Zhelannikov A.I., Zamyatin A.N. Modelirovanie vzaimodeyjstviya kondensacionnogo i vikhrevogo sledov za vozdushnihmi sudami [Modeling the interaction of condensation and vortex wakes behind aircraft. Scientific Bulletin MSTUCA]. Moscow. Nauchnihyj vestnik MGTU GA. 2015. № 212. PP. 5 – 10. (In Russian)
Review
For citations:
Zhelannikov A.I. FEATURES OF SPREAD OF VORTEX WAKE BEHIND AIRCRAFT AT TAKEOFF AND LANDING, IF CROSSWINDS. Civil Aviation High Technologies. 2016;(223):5-11. (In Russ.)
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