Approximate computational model for the local postbuckling of omega‐stringer‐stiffened composite panels

نویسندگان

چکیده

Abstract Typical thin‐walled structures are found in applications like aircraft, spacecraft and marine vessels. For this type of structure, stability behaviour is crucial. The better understood, the full lightweight potential can be exploited. composite especially, new fast analysis tools for preliminary design required to address issue. Therefore, local postbuckling omega‐stringer‐stiffened panels subject a computational model. method computationally highly efficient because it based on closed‐form analytical approach. explicit solution derived principle minimum total elastic potential. Furthermore, assumes that initial eigenform does not substantially change early regime. In way, plates skin stringer included explicitly analysis. Compared finite element model literature, tool assessed. results indicate excellent agreement panels, where bay plate most critical panel. promises framework.

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ژورنال

عنوان ژورنال: Proceedings in applied mathematics & mechanics

سال: 2023

ISSN: ['1617-7061']

DOI: https://doi.org/10.1002/pamm.202200152