Abstract
The present paper solves the arrangement of the wing and fuselage structures with respect to the relative position of the large cutouts in both airframe parts. The finite element method based on displacement field is used for the analysis of wing structure ,while the matrix force method as given by Prof. Argyris is used for the analysis of fuselage structure. A computer program for the combined displacement-force method is constructed. Numerical examples, representing different arrangements are included which illustrate the application of the method to practical problems.The ciculated results are compared with those obtained by measurements.
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 callMore From: The International Conference on Applied Mechanics and Mechanical Engineering
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.
