POSSIBILITY OF CIVIL AIRCRAFT IN-FLIGHT REFUELING
Abstract
With application of the developed calculation-software package there were conducted the researches, demonstrating the possibility of in-flight refueling of civil aircraft. As a flying tanker there were chosen tanker aircraft ILyushin-78 which is currently operated and a perspective tanker on the basis of ILyushin-96-400T aircraft. Perspective aircraft MC-21-400 was chosen as an aircraft to be refueled.
About the Authors
A. I. Zhelannikov
ЦАГИ им. Н.Е. Жуковского
Russian Federation
Russian Federation
A. N. Zamyatin
НИО-2 ЛИИ им. М.М. Громова
Russian Federation
Russian Federation
References
1. Zhelannikov A.I., Zamyatin A.N. Svideteljstvo o gosudarstvennoyj registracii programmih dlya EhVM №2015614783 "Raschetno-programmnihyj kompleks dlya sistemih vikhrevoyj bezopasnosti" [Certificate of state registration of the computer software "The calculation-software package for system of vortex safety"] 2015.
2. Zhelannikov A.I. Osobennosti rasprostraneniya vikhrevogo sleda za vozdushnihmi sudami na rezhimakh vzleta i posadki pri nalichii bokovogo vetra [Features of spread of vortex wake behind aircraft at takeoff and landing, if crosswinds. Scientific Bulletin MSTUCA]. Moscow. Nauchnihyj vestnik MGTU GA. 2016. № 223. PP. 5 – 11. (In Russian)
3. Aubakirov T.O., Zhelannikov A.I., Ivanov P.E., Nisht M.I. Sputnihe sledih i ikh vozdeyjst-vie na letateljnihe apparatih. Modelirovanie na EhVM [Co-current traces and their impact on aircraft. Modeling on the computer]. Almaty. 1999. 230 p. (In Russian)
4. Ginevskiyj A.S., Zhelannikov A.I. Vikhrevihe sledih samoletov [Vortex traces of planes]. Moscow. Fizmatlit, 2008. 170 p. (In Russian)
5. 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)
6. 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)
7. 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)
8. 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)
9. 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., Zamyatin A.N. POSSIBILITY OF CIVIL AIRCRAFT IN-FLIGHT REFUELING. Civil Aviation High Technologies. 2016;(223):12-18. (In Russ.)
Views:
555
Email this article 
