Abstract
ABSTRACT This paper presents the study on vibration characteristics of an aircraft wing. A300 aircraft wing with NACA 64215 aerofoil is used for this investigation. A computer-aided design model of the wing is created by using CATIA V5 R20 and analyses are done by utilising ANSYS workbench 16.0. The analysis has been done on the wing by considering one end (root chord) of the wing is fixed while the other end (tip chord) is free. A numerical validation procedure is done by workbench and finite element analysis software with the structural analysis and model analysis is carried out to find the total deformation and frequency of wing without and with winglet with different angles. Wing with 18° and 45° inclination of winglet have been taken for study. The deformation and stress acting on the model of wing with and without winglet have been studied.
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.
