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Mixed plate theories based on the Generalized Unified Formulation. Part IV: Zig-zag theories

Composite structures, 2009-02, Vol.87 (3), p.195-205

Demasi, Luciano

2009

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Partially Layer Wise advanced Zig Zag and HSDT models based on the Generalized Unified Formulation

Engineering structures, 2013-08, Vol.53, p.63-91

Demasi, Luciano

2013

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A hierarchical generalized formulation for the large-displacement dynamic analysis of rotating plates

Computational mechanics, 2021-12, Vol.68 (6), p.1325-1347

2021

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Mixed plate theories based on the Generalized Unified Formulation. Part V: Results

Composite structures, 2009-03, Vol.88 (1), p.1-16

Demasi, Luciano

2009

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Challenges, Ideas, and Innovations of Joined-Wing Configurations: A Concept from the Past, an Opportunity for the Future

Progress in aerospace sciences, 2016-11, Vol.87, p.1-93

2016

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Properties and layerwise modeling of the Harlequin variational theorem for composite structures

Mechanics of advanced materials and structures, 2023-10, p.1-30

Demasi, Luciano

2023

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Partitioned parametrized variational procedure for the generation of theorems of structural analysis

Mechanics of advanced materials and structures, 2023-05, Vol.30 (9), p.1749-1768

Demasi, Luciano

2023

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Mixed plate theories based on the Generalized Unified Formulation. Part III: Advanced mixed high order shear deformation theories

Composite structures, 2009-02, Vol.87 (3), p.183-194

Demasi, Luciano

2009

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Partially Zig-Zag Advanced Higher Order Shear Deformation Theories Based on the Generalized Unified Formulation

Composite structures, 2012, Vol.94 (2), p.363-375

Demasi, Luciano

2012

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Large displacement models for composites based on Murakami's Zig-Zag Function, Green-Lagrange Strain Tensor, and Generalized Unified Formulation

Thin-walled structures, 2020-05, Vol.150, p.106460, Article 106460

2020

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Properties and numerical solution of an integral equation system to minimize airplane drag for a multiwing system

Mathematical methods in the applied sciences, 2024-09, Vol.47 (13), p.11062-11085

2024

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Refined multilayered plate elements based on Murakami zig–zag functions

Composite structures, 2005-09, Vol.70 (3), p.308-316

Demasi, Luciano

2005

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Equivalent Single Layer, Zig-Zag, and Layer Wise theories for variable angle tow composites based on the Generalized Unified Formulation

Composite structures, 2017-10, Vol.177, p.54-79

2017

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A refined structural model for static aeroelastic response and divergence of metallic and composite wings

CEAS aeronautical journal, 2013-06, Vol.4 (2), p.175-189

2013

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Reissner’s Mixed Variational Theorem and triangular finite element discretizations: an energetic interpretation

Thin-walled structures, 2021-09, Vol.166, p.107994, Article 107994

2021

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Assess the Accuracy of the Variational Asymptotic Plate and Shell Analysis Using the Generalized Unified Formulation

Mechanics of advanced materials and structures, 2013-03, Vol.20 (3), p.227-241

2013

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Exploratory Structural Investigation of a Hawkmoth-Inspired MAV's Thorax

International journal of micro air vehicles, 2012-12, Vol.4 (4), p.291-304

2012

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Investigation on the Conditions of Minimum Induced Drag of Closed Wing Systems and C-Wings

Journal of aircraft, 2007-01, Vol.44 (1), p.81-99

Demasi, Luciano

2007

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2D, Quasi 3D and 3D Exact Solutions for Bending of Thick and Thin Sandwich Plates

The journal of sandwich structures & materials, 2008-07, Vol.10 (4), p.271-310

Demasi, Luciano

2008

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Treatment of stress variables in advanced multilayered plate elements based upon Reissner’s mixed variational theorem

Computers & structures, 2006-07, Vol.84 (19), p.1215-1221

Demasi, Luciano

2006

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

Composite structures, 2015-11, Vol.131, p.501-515

2015

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Minimum Induced Drag Theorems for Joined Wings, Closed Systems, and Generic Biwings: Applications

Journal of optimization theory and applications, 2016-04, Vol.169 (1), p.236-261

2016

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Quasi-3D analysis of free vibration of anisotropic plates

Composite structures, 2006-08, Vol.74 (4), p.449-457

Demasi, Luciano

2006

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Minimum Induced Drag Theorems for Joined Wings, Closed Systems, and Generic Biwings: Theory

Journal of optimization theory and applications, 2016-04, Vol.169 (1), p.200-235

2016

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Classical and advanced multilayered plate elements based upon PVD and RMVT. Part 1: Derivation of finite element matrices

International journal for numerical methods in engineering, 2002-09, Vol.55 (2), p.191-231

2002

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Mixed plate theories based on the Generalized Unified Formulation. Part IV: Zig-zag theories

Partially Layer Wise advanced Zig Zag and HSDT models based on the Generalized Unified Formulation

A hierarchical generalized formulation for the large-displacement dynamic analysis of rotating plates

Mixed plate theories based on the Generalized Unified Formulation. Part V: Results

Challenges, Ideas, and Innovations of Joined-Wing Configurations: A Concept from the Past, an Opportunity for the Future

Properties and layerwise modeling of the Harlequin variational theorem for composite structures

Partitioned parametrized variational procedure for the generation of theorems of structural analysis

Mixed plate theories based on the Generalized Unified Formulation. Part III: Advanced mixed high order shear deformation theories

Partially Zig-Zag Advanced Higher Order Shear Deformation Theories Based on the Generalized Unified Formulation

Large displacement models for composites based on Murakami's Zig-Zag Function, Green-Lagrange Strain Tensor, and Generalized Unified Formulation

Properties and numerical solution of an integral equation system to minimize airplane drag for a multiwing system

Refined multilayered plate elements based on Murakami zig–zag functions

Equivalent Single Layer, Zig-Zag, and Layer Wise theories for variable angle tow composites based on the Generalized Unified Formulation

A refined structural model for static aeroelastic response and divergence of metallic and composite wings

Reissner’s Mixed Variational Theorem and triangular finite element discretizations: an energetic interpretation

Assess the Accuracy of the Variational Asymptotic Plate and Shell Analysis Using the Generalized Unified Formulation

Exploratory Structural Investigation of a Hawkmoth-Inspired MAV's Thorax

Investigation on the Conditions of Minimum Induced Drag of Closed Wing Systems and C-Wings

2D, Quasi 3D and 3D Exact Solutions for Bending of Thick and Thin Sandwich Plates

Treatment of stress variables in advanced multilayered plate elements based upon Reissner’s mixed variational theorem

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

Minimum Induced Drag Theorems for Joined Wings, Closed Systems, and Generic Biwings: Applications

Quasi-3D analysis of free vibration of anisotropic plates

Minimum Induced Drag Theorems for Joined Wings, Closed Systems, and Generic Biwings: Theory

Classical and advanced multilayered plate elements based upon PVD and RMVT. Part 1: Derivation of finite element matrices

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