A generalized, multilength scale framework for thermo-diffusional-mechanically coupled, nonlinear, laminated plate theories with delaminations

Williams, Todd O.

doi:10.1016/j.ijsolstr.2004.08.007

Cited by 23 publications

(12 citation statements)

References 32 publications

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“…Particularly interesting is the formulation proposed by Todd Williams (Refs. [69][70][71]) in which Equivalent-Single-Layer approaches and Layer-Wise ones coexist in the same theoretical framework. Another option, on which the present effort is based upon, is represented by the so-called Compact Notations (CNs) (see Ref.…”

Section: Reissner Multilayered Theory (Rmt)mentioning

confidence: 99%

Generalized Unified Formulation shell element for functionally graded Variable-Stiffness Composite Laminates and aeroelastic applications

Demasi

Ashenafi

Cavallaro

et al. 2015

Composite Structures

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Section: Reissner Multilayered Theory (Rmt)mentioning

confidence: 99%

Generalized Unified Formulation shell element for functionally graded Variable-Stiffness Composite Laminates and aeroelastic applications

Demasi

Ashenafi

Cavallaro

et al. 2015

Composite Structures

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“…His major effort concerns with global-local approach. In [64] he proposed a new plate theory which is based on a general, unified, theoretical framework for the response of nonlinear, delaminated plate theories in the presence of thermo-diffusional-mechanical coupling. A general, theoretical framework for the development of comprehensive, nonlinear, multiscale plate theories for laminated structures is suggested in Ref.…”

Section: Full Layer-wise Plate Theory With Interface Layermentioning

confidence: 99%

Intra and damage analysis of laminated composites using coupled continuum damage mechanics with cohesive interface layer

Mohammadi

Olia

Hosseini‐Toudeshky

2015

Composite Structures

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“…Generally, three length scales can be used for the analysis of heterogeneous materials [121,122]. Each length scale is interacting with each other.…”

Section: Modeling Scale Levelsmentioning

confidence: 99%

Identification of the local stiffness reduction of a damaged composite plate using the virtual fields method

Kim

Pierron

Wisnom

et al. 2007

Composites Part A: Applied Science and Manufacturing

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For the purpose of returning to Earth And I do not call one a Brahmana on account of his birth or of his origin from (a particular) mother; (but) the one who is possessed of nothing and seizes upon nothing, him I call a Brahmana.The man who is free from anger, endowed with (holy) works, virtuous, without desire, subdued, and wearing the last body (antimasarira), him I call a Brahmana.The man who is not hostile amongst the hostile, who is peaceful amongst the violent, not seizing (upon anything) amongst those that seize (upon everything), him I call a Brahmana.Whosoever has passed over this quagmire dicult to pass, (who has passed over) revolution (samsara) and folly, who has crossed over, who has reached the other shore, who is meditative, free from desire and doubt, calm without seizing (upon anything), him I call a Brahmana. Sutta Nipata, Book 3, Chapter 9 AcknowledgementsThis thesis is the record of my four years' exploration into a new world and myself.

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A generalized, multilength scale framework for thermo-diffusional-mechanically coupled, nonlinear, laminated plate theories with delaminations

Cited by 23 publications

References 32 publications

Generalized Unified Formulation shell element for functionally graded Variable-Stiffness Composite Laminates and aeroelastic applications

Generalized Unified Formulation shell element for functionally graded Variable-Stiffness Composite Laminates and aeroelastic applications

Intra and damage analysis of laminated composites using coupled continuum damage mechanics with cohesive interface layer

Identification of the local stiffness reduction of a damaged composite plate using the virtual fields method

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