2018
DOI: 10.1016/j.marstruc.2018.01.001
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A new method to estimate ultimate strength of stiffened panels under longitudinal thrust based on analytical formulas

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Cited by 27 publications
(8 citation statements)
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“…This evaluation is conducted for different sub-domains. It was suggested by Ozdemir et al (2018) that the primary failure mode of stiffened panels under compression may change from local plate buckling to beam-column buckling at the threshold λ = 0.6. On the other hand, the compressive strength of plating may change substantially when β > 1.9.…”
Section: Evaluation Of Existing Empirical Methodsmentioning
confidence: 99%
“…This evaluation is conducted for different sub-domains. It was suggested by Ozdemir et al (2018) that the primary failure mode of stiffened panels under compression may change from local plate buckling to beam-column buckling at the threshold λ = 0.6. On the other hand, the compressive strength of plating may change substantially when β > 1.9.…”
Section: Evaluation Of Existing Empirical Methodsmentioning
confidence: 99%
“…This might represent a constraint on the deformation of the plate and on the web and flange of the stiffener, but the experience from other similar analyses [9,10] indicates that this has small impact on the results. Edge B2 is fixed in the 1-direction.…”
Section: Finite Element Model (Fem)mentioning
confidence: 99%
“…Ozdemir et al [10] proposed a new approximate method based on analytical formulas to estimate the ultimate strength of stiffened panels, where a series of detailed elastoplastic large deflection FEA was carried out. The initial deflections were accounted for in the form of thin-horse mode plus overall buckling mode for the plates, and flexural buckling mode plus tripping mode for the stiffeners.…”
Section: Introductionmentioning
confidence: 99%
“…Ozdemir et al [101] proposed a new method to predict the ultimate load capacity of the stiffened panels using the large elastic and initial yield solution. The proposed model was shown to be good enough to predict the ultimate load capacity of the stiffened panels compared with finite element solutions.…”
Section: Collapse Strength Assessmentmentioning
confidence: 99%