Abstract
This work relates to the formulation of finite strip for the analysis of thin circular cylindrical shells. The thin shell supported on diaphragms at circular ends has been taken for the analysis by finite strip method. The diaphragms are infinitely rigid in their own planes and flexible perpendicular to the plane. The behavior of thin cylindrical shell is governed by Love-Kirchhoff assumptions. Koiter’s [1] theory of thin cylindrical shell is used as a base for the derivation of strain components. The discretization of half shell has been done in to finite strips are taken along the length of the shell.
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.
