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MATHEMATICAL MODEL OF THE AIRCRAFT AERODYNAMICS IN A VORTEX WAKE

卷 49, 册 4, 2018, pp. 437-453
DOI: 10.1615/TsAGISciJ.2018027647
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摘要

The process of the generation and evolution of the vortex wake behind an aircraft in turbulent atmosphere is considered. An artificial neural networks–based approach to the development of a mathematical model of the aerodynamics of an aircraft during in-flight refueling is proposed. The accuracy and speed of the developed software module were evaluated for the problem of in-flight refueling modeling using a ground-based flight simulator.

参考文献
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