Abstract
This paper reviews and evaluates the most recent studies on forward-swept wing technology. A number of experimental plans and applications for forward-swept wing aircraft have been produced as a result of the study of forward-swept wings, the investigation of aerodynamic circumstances, and the creation of related designs. The related theories and exposed problems of the forward-swept wing aircraft, such as the problem of aeroelastic divergence, structural strength, and the descent of transonic flight state, are gradually solved. It will be demonstrated that forward-swept wing aircraft have outstanding aerodynamic performance in subsonic flight. In comparison to current aircraft, it may gain more controllability advantages, enhance low-speed controllability, increase aerodynamic efficiency in a variety of flying scenarios, decrease stall speed, making the aircraft less likely to enter the spiral state, and increase safety and dependability. The research in the field of forward swept wing will increase the possibility of successful development and practical use of forward swept wing aircraft.
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.
