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JOURNALS // Prikladnaya Mekhanika i Tekhnicheskaya Fizika // Archive

Prikl. Mekh. Tekh. Fiz., 2019 Volume 60, Issue 2, Pages 148–157 (Mi pmtf466)

This article is cited in 5 papers

Modeling of aircraft flight through the wake vortex

A. M. Gaifullin, O. V. Animitsa, I. S. Bosnyakov, P. V. Kuzmin, Yu. N. Sviridenko, S. N. Suprunenko, K. G. Khairullin

Central Aerohydrodynamic Institute, Zhukovsky, 140180, Russia

Abstract: A mathematical model is proposed for calculating the forces and moments acting on an aircraft in the region affected by the wake vortex generated by another aircraft. This model takes into account various random factors and determines the wake vortex characteristics, as well as its shape, which depends on integral and distributed characteristics of atmospheric turbulence. The computational scheme, which involves the use of artificial neural networks, allows real-time calculation of the aerodynamic characteristics of the aircraft and to ensure training of pilots on flight simulators.

Keywords: wake vortex, artificial neural networks, aerodynamic characteristics, flight simulators.

UDC: 532.527: 629.7

Received: 16.10.2018
Revised: 16.10.2018
Accepted: 29.10.2018

DOI: 10.15372/PMTF20190212


 English version:
Journal of Applied Mechanics and Technical Physics, 2019, 60:2, 314–322

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