Stress analysis of corrugated orthotropic laminates under transverse shear loading

Filipovic, Daniel; Kress, Gerald

doi:10.1016/j.compstruct.2019.110983

Cited by 6 publications

(3 citation statements)

References 14 publications

Supporting

Mentioning

Contrasting

Order By: Relevance

“…where the left subscript t denotes the incremental value. Substituting Eq (9) into the incremental stress-strain relationship, t S l ij = t C l ijrs t l rs , the incremental PK2 tensor and then Cauchy stress tensor can be also rewritten as follows:…”

Section: Finite Element Formulationmentioning

confidence: 99%

See 1 more Smart Citation

Interlaminar stress analysis of composite shell structures using a geometrically nonlinear layer-wise shell finite element

Soltani

Kordkheili

2021

Composite Structures

View full text Add to dashboard Cite

This work aims to calculate interlaminar stress distribution through the thickness of multilayered composite shell structures by employing a novel nonlinear layer-wise shell finite element formulation. Adapting the Mindlin-Reissner theory in each layer, the shear-deformable layer-wise shell element presents the interlaminar shear stress distributions by increasing the number of layers. The interlaminar normal stress distribution is then determined by the finite difference solution of the general form of equilibrium equation in the non-orthogonal curvilinear grid along the Gaussian points. Two boundary conditions at the bottom and the top surfaces are satisfied by adopting the linear Lagrange interpolation function. The developed formulation is assessed through some illustrative problems solved using a proprietary finite element computer program. The results compare very well with those available in the literature and those obtained by simulations with the commercial finite element software Ansys.

show abstract

Section: Finite Element Formulationmentioning

confidence: 99%

“…Interlaminar stress in corrugated laminates studied by Thurnherr et al [8]. Filipovic and Kress [9] studied the stress distribution in corrugated orthotropic laminates under shear loading.…”

Section: Introductionmentioning

confidence: 99%

Interlaminar stress analysis of composite shell structures using a geometrically nonlinear layer-wise shell finite element

Soltani

Kordkheili

2021

Composite Structures

View full text Add to dashboard Cite

show abstract

“…Kress and Winkler [23] derived the analytical expressions of the equivalent orthotropic plate when the corrugations are defined as circular arcs. A planar finite element was developed [24], and the transverse shear response was also taken into account by Filipovic and Kress [25,26]. Dayyani et al [27] investigated the tensile and flexural properties of corrugated laminate panels using numerical and experimental methods.…”

Section: Introductionmentioning

confidence: 99%

Predicting global strain limits for corrugated panels

Wang

Xia

Friswell

et al. 2020

Composite Structures

View full text Add to dashboard Cite

This is a PDF file of an article that has undergone enhancements after acceptance, such as the addition of a cover page and metadata, and formatting for readability, but it is not yet the definitive version of record. This version will undergo additional copyediting, typesetting and review before it is published in its final form, but we are providing this version to give early visibility of the article. Please note that, during the production process, errors may be discovered which could affect the content, and all legal disclaimers that apply to the journal pertain.

show abstract

Equivalent orthotropic model for corrugated plates based on simplified constitutive relation

Lang

2022

Heliyon

View full text Add to dashboard Cite

Stress analysis of corrugated orthotropic laminates under transverse shear loading

Cited by 6 publications

References 14 publications

Interlaminar stress analysis of composite shell structures using a geometrically nonlinear layer-wise shell finite element

Interlaminar stress analysis of composite shell structures using a geometrically nonlinear layer-wise shell finite element

Predicting global strain limits for corrugated panels

Equivalent orthotropic model for corrugated plates based on simplified constitutive relation

Contact Info

Product

Resources

About