Abstract

In the design process of an aircraft, there is an important criterion to consider when designing a wing: how much lift the wing can provide. The magnitude of the lift directly determines the stability of the aircraft during take-off and whether it can take off smoothly, so it has received extensive attention from scholars at home and abroad. This paper uses the Kutta-Joukowski theorem to quantify the factors that affect wing lift and enable the calculation of lift, and engineers need to analyze how these factors affect wing lift when considering this criterion. So how can engineers analyze the effect of these factors on lift, especially in multivariate situations? Need to calculate complex multivariate equations? are issues worth exploring. In this paper, a coupled analysis method is proposed to analyze the wing lift of an aircraft affected by multiple variables, which will greatly simplify the original analysis process and provide convenience for the calculation of wing lift.

Full Text
Paper version not known

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 call

Disclaimer: 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.