Abstract
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.
Sign-in/Register to access full text options 
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have
Schedule a callDisclaimer: All third-party content on this website/platform is and will remain the property of their respective owners and is provided on "as is" basis without any warranties, express or implied. Use of third-party content does not indicate any affiliation, sponsorship with or endorsement by them. Any references to third-party content is to identify the corresponding services and shall be considered fair use under The CopyrightLaw.
