Abstract
E FUSELAGE has several cutouts, the largest, of course, being those for cabin doors. These cutouts cause considerable changes in the distribution of shear stresses due to torsion and additional axial forces in the stringers. This paper presents a method of solving the stated problem. In order to obtain a simple solution of this statically indeterminate problem, the following assumptions are made:f (a) the stringers plus effective width of skin carry only axial forces; and (b) the skin between the stringers is subjected to shear stresses only.
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.
