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AIRCRAFT-CARRIER VORTEX WAKE CALCULATIONS

Abstract

Calculations of the perturbed velocity field and induced turbulence due to the motion of the ship in the atmospheric surface layer based on gradient wind are presented in this paper.

About the Authors

I. S. Bosnyakov
ЦАГИ
Russian Federation


A. A. Kornyakov
ЦАГИ
Russian Federation


G. G. Soudakov
ЦАГИ, МФТИ
Russian Federation


References

1. Polsky S.A. A computational study of unsteady ship airwake. AIAA 2002-1022. 2002. P. 11.

2. Bobylev A.V., Vyshinsky V.V., Soudakov G.G., Yaroshevsky V.A. Aircraft Vortex Wake and Flight Safety Problems. Journal of Aircraft. Vol. 47. № 2. March–April 2010.

3. Vihshinskiyj V.V., Sudakov G.G. Vihrevoj sled samoleta v turbulentnoj atmosphere. Trudih CAGI. 2005. Vihp. 2667. P. 155. (In Russian).

4. Garbaruk A.V., Strelec M.Kh., Shur M.L. Modelirovanie turbulentnosti v raschetakh slozhnihkh techeniyj: uchebnoe posobie. SPb.: Izd-vo Politekhn. un-ta. 2012. 88 p. (In Russian).

5. Landau L.D., Lifshic E.M. Teoreticheskaya fizika. Gidrodinamika. M.: Nauka. 1988. T. 6. 736 p. (In Russian).


Review

For citations:


Bosnyakov I.S., Kornyakov A.A., Soudakov G.G. AIRCRAFT-CARRIER VORTEX WAKE CALCULATIONS. Civil Aviation High Technologies. 2015;(212):55-59. (In Russ.)

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ISSN 2079-0619 (Print)
ISSN 2542-0119 (Online)