Theoretical calculation method of hyperbolic rotating thin shell bending problem

ObjectiveIn order to analyze the bending characteristics of a hyperbolic rotating thin shell, the complex two-dimensional mechanical problem is simplified into a one-dimensional bending problem based on Euler's Bernoulli beam theory. MethodBy analyzing the force and deformation characteristics of shells and belt beams, a structural mechanical model is established, and a double curvature rotating thin shell bending differential equation is obtained by combining the physical equation of plate and shell theory with the bending differential equation of a single-span beam. An empirical formula for typical stress is proposed and its accuracy verified by an ANSYS-based simulation. ResultsThe results show that the error between the simulation and the formula is about 2.3%, which demonstrates the high accuracy of the formula in predicting typical stress and verifies the correctness of the theoretical calculation method. ConclusionThe proposed method can provide useful references for the design and optimization of similar structure.

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Publication Details

Journal
SHILAP Revista de lepidopterología
Published
2025-04-01
DOI
https://doi.org/10.19693/j.issn.1673-3185.03594
Primary Topic
Influenza Virus Research Studies
Type
article
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article

Theoretical calculation method of hyperbolic rotating thin shell bending problem

SHILAP Revista de lepidopterología
Influenza Virus Research Studies
article

Theoretical calculation method of hyperbolic rotating thin shell bending problem

article en

Abstract

ObjectiveIn order to analyze the bending characteristics of a hyperbolic rotating thin shell, the complex two-dimensional mechanical problem is simplified into a one-dimensional bending problem based on Euler's Bernoulli beam theory. MethodBy analyzing the force and deformation characteristics of shells and belt beams, a structural mechanical model is established, and a double curvature rotating thin shell bending differential equation is obtained by combining the physical equation of plate and shell theory with the bending differential equation of a single-span beam. An empirical formula for typical stress is proposed and its accuracy verified by an ANSYS-based simulation. ResultsThe results show that the error between the simulation and the formula is about 2.3%, which demonstrates the high accuracy of the formula in predicting typical stress and verifies the correctness of the theoretical calculation method. ConclusionThe proposed method can provide useful references for the design and optimization of similar structure.

SHILAP Revista de lepidopterología
Naval University of Engineering (CN)
Sustainable cities and communities
Openalex Percentile: Top 44%
Influenza Virus Research Studies
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Theoretical calculation method of hyperbolic rotating thin shell bending problem · SHILAP Revista de lepidopterología (2025) | TGRS Research Map | TGRS