Modeling of Aircraft Flight Through the Wake Vortex


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详细

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.

作者简介

A. Gaifullin

Central Aerohydrodynamic Institute

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Email: gaifullin@tsagi.ru
俄罗斯联邦, Zhukovsky, 140180

O. Animitsa

Central Aerohydrodynamic Institute

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Email: flight15@tsagi.ru
俄罗斯联邦, Zhukovsky, 140180

I. Bosnyakov

Central Aerohydrodynamic Institute

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Email: bossig@yandex.ru
俄罗斯联邦, Zhukovsky, 140180

P. Kuzmin

Central Aerohydrodynamic Institute

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Email: piter_VK@mail.ru
俄罗斯联邦, Zhukovsky, 140180

Yu. Sviridenko

Central Aerohydrodynamic Institute

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Email: ysviridenko@yandex.ru
俄罗斯联邦, Zhukovsky, 140180

S. Suprunenko

Central Aerohydrodynamic Institute

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Email: slava-PC@yandex.ru
俄罗斯联邦, Zhukovsky, 140180

K. Khairullin

Central Aerohydrodynamic Institute

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Email: khayrullin.kamil@gmail.com
俄罗斯联邦, Zhukovsky, 140180

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