Abstract
This paper is concerned with a numerical prediction of geometrically nonlinear behaviors of shallow (hyperbolic paraboloidal) shell models with clamped edges subjected to air pressures. The numerical analysis of the experimental models in the previous work [6] is carried out in detail with the use of higher order finite difference approximations by taking into account the effects of initial configurations of shell models. A considerably close agreement between almost all the numerical and experimental data except some local data verifies the accuracy and reliability of the present method and solution at least with respect to the benchmark load-deflection curves of the particular cases treated here.
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: Transactions of the Architectural Institute of Japan
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.
