Parametric study on average stress-average strain curve of composite stiffened plates using progressive failure method

The post-buckling behavior of composite ships' stiffened plate panels has been studied. In this study, the average strain- average stress curves for these panels are derived using progressive failure method as well as nonlinear finite element method. The boundary conditions are appropriate for...

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Main Authors: Fattaneh Morshedsolouk, Mohammad Reza Khedmati
Format: Article
Language:English
Published: Marcílio Alves
Series:Latin American Journal of Solids and Structures
Subjects:
Online Access:http://www.scielo.br/scielo.php?script=sci_arttext&pid=S1679-78252014001200005&lng=en&tlng=en
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author Fattaneh Morshedsolouk
Mohammad Reza Khedmati
author_facet Fattaneh Morshedsolouk
Mohammad Reza Khedmati
author_sort Fattaneh Morshedsolouk
collection DOAJ
description The post-buckling behavior of composite ships' stiffened plate panels has been studied. In this study, the average strain- average stress curves for these panels are derived using progressive failure method as well as nonlinear finite element method. The boundary conditions are appropriate for the continuous plate panels used in shipbuilding. The effects of the aspect ratio, initial geometrical imperfection and stiffener size on the post-buckling of these stiffened panels are evaluated
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spelling doaj.art-bc773fbf22074680b64ce822fd4167d62022-12-22T00:04:59ZengMarcílio AlvesLatin American Journal of Solids and Structures1679-782511122203222610.1590/S1679-78252014001200005S1679-78252014001200005Parametric study on average stress-average strain curve of composite stiffened plates using progressive failure methodFattaneh Morshedsolouk0Mohammad Reza Khedmati1Amirkabir University of TechnologyAmirkabir University of TechnologyThe post-buckling behavior of composite ships' stiffened plate panels has been studied. In this study, the average strain- average stress curves for these panels are derived using progressive failure method as well as nonlinear finite element method. The boundary conditions are appropriate for the continuous plate panels used in shipbuilding. The effects of the aspect ratio, initial geometrical imperfection and stiffener size on the post-buckling of these stiffened panels are evaluatedhttp://www.scielo.br/scielo.php?script=sci_arttext&pid=S1679-78252014001200005&lng=en&tlng=enProgressive failure analysishat stiffened plate panelinitial imperfectionFinite Element Method
spellingShingle Fattaneh Morshedsolouk
Mohammad Reza Khedmati
Parametric study on average stress-average strain curve of composite stiffened plates using progressive failure method
Latin American Journal of Solids and Structures
Progressive failure analysis
hat stiffened plate panel
initial imperfection
Finite Element Method
title Parametric study on average stress-average strain curve of composite stiffened plates using progressive failure method
title_full Parametric study on average stress-average strain curve of composite stiffened plates using progressive failure method
title_fullStr Parametric study on average stress-average strain curve of composite stiffened plates using progressive failure method
title_full_unstemmed Parametric study on average stress-average strain curve of composite stiffened plates using progressive failure method
title_short Parametric study on average stress-average strain curve of composite stiffened plates using progressive failure method
title_sort parametric study on average stress average strain curve of composite stiffened plates using progressive failure method
topic Progressive failure analysis
hat stiffened plate panel
initial imperfection
Finite Element Method
url http://www.scielo.br/scielo.php?script=sci_arttext&pid=S1679-78252014001200005&lng=en&tlng=en
work_keys_str_mv AT fattanehmorshedsolouk parametricstudyonaveragestressaveragestraincurveofcompositestiffenedplatesusingprogressivefailuremethod
AT mohammadrezakhedmati parametricstudyonaveragestressaveragestraincurveofcompositestiffenedplatesusingprogressivefailuremethod