J.L. Curiel-Sosa
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View article: Robust Fast Fracture Plane Orientation Angle Search Algorithm for Puck 3D Inter-Fibre Failure Criterion
Robust Fast Fracture Plane Orientation Angle Search Algorithm for Puck 3D Inter-Fibre Failure Criterion Open
In the present work, a novel fast fracture plane orientation angle (FPOA) search algorithm for the 3D Puck failure criterion is proposed. In the 3D Puck failure criterion, a linear search algorithm is employed to calculate the maximum inte…
View article: Micromechanical Computational Analysis of Debonding and Kinking in Microscale Composites
Micromechanical Computational Analysis of Debonding and Kinking in Microscale Composites Open
Composites are widely utilized across various industries due to their exceptional properties, allowing design flexibility and complexity. There are different scales of composites numerical study, and this study aims to understand the damag…
View article: Damage in hybrid corrugated core sandwich structures under high velocity hail ice impact: A numerical study
Damage in hybrid corrugated core sandwich structures under high velocity hail ice impact: A numerical study Open
Potential damage in composite structures caused by hail ice impact is an essential safety threat to the aircraft in flight. In this study, a nonlinear finite element (FE) model is developed to investigate the dynamic response and damage be…
View article: Evaluation on Piezoaeroelastic Energy Harvesting Potential of A Jet Transport Aircraft Wing with Multiphase Composite by means of Iterative Finite Element Method
Evaluation on Piezoaeroelastic Energy Harvesting Potential of A Jet Transport Aircraft Wing with Multiphase Composite by means of Iterative Finite Element Method Open
This paper presents new insight on the potential of piezoaeroelastic energy harvesting on the transport aircraft wing structure. A novel numerical investigation is conducted in the present study. An advanced iterative finite element method…
View article: A Novel Finite Element Method Approach in the Modelling of Edge Trimming of CFRP Laminates
A Novel Finite Element Method Approach in the Modelling of Edge Trimming of CFRP Laminates Open
Nowadays, the development of robust finite element models is vital to research cost-effectively the optimal cutting parameters of a composite machining process. However, various factors, such as the high computational cost or the complicat…
View article: Meshfree analysis of functionally graded plates with a novel four-unknown arctangent exponential shear deformation theory
Meshfree analysis of functionally graded plates with a novel four-unknown arctangent exponential shear deformation theory Open
A novel refined arctangent exponential shear deformation theory (RAESDT) is presented for analysis the mechanical behavior of both isotropic and sandwich FGM plates. Material properties are set to be isotropic at each point and varied acro…
View article: Computational Modelling of Failure Mechanisms in Fibre Metal Laminates
Computational Modelling of Failure Mechanisms in Fibre Metal Laminates Open
View article: Comparison of Computational Techniques for Prediction of Delamination Initiation and Propagation in Composite Laminates
Comparison of Computational Techniques for Prediction of Delamination Initiation and Propagation in Composite Laminates Open
In the past few decades, interlaminar and intralaminar damage interaction on composite laminates has been extensively investigated in order to predict failure.It is widely known that predictive modelling of composite structures failure -sp…
View article: Numerical analysis of the delamination in CFRP laminates: VCCT and XFEM assessment
Numerical analysis of the delamination in CFRP laminates: VCCT and XFEM assessment Open
View article: Unsteady shock front waviness in shock-buffet of transonic aircraft
Unsteady shock front waviness in shock-buffet of transonic aircraft Open
The unsteady transonic aerodynamics of a wing-body configuration is investigated by solving the Unsteady Reynolds-averaged Navier-Stokes equations closed with the full Reynolds Stress Model. This work presents the prediction of flow field …
View article: Study of the machining induced damage in UD-CFRP laminates with various fibre orientations: FE assessment
Study of the machining induced damage in UD-CFRP laminates with various fibre orientations: FE assessment Open
Finite elements (FE) provide an excellent and low-cost approach in the assessment of composite machining induced damage. This article is focused on the evaluation of the damage underlying the machined surface through the development of a n…
View article: Machining induced damage in orthogonal cutting of UD composites: FEA based assessment of Hashin and Puck criteria
Machining induced damage in orthogonal cutting of UD composites: FEA based assessment of Hashin and Puck criteria Open
FE models offer a promising virtual alternative to study machining responses of composites, thereby allowing an informed selection of favorable cutting parameters. Appropriate mathematical schemes are needed to predict damage initiation in…
View article: Chip formation in machining of unidirectional carbon fibre reinforced polymer laminates: FEM based assessment
Chip formation in machining of unidirectional carbon fibre reinforced polymer laminates: FEM based assessment Open
Finite-element (FE) method offers a low cost virtual alternative to assist in optimisation of critical process parameters in machining of composites. This study is focussed on understanding the mechanics of chip formation in orthogonal cut…
View article: Numerical Inspection based on Quasi-Static Analysis using Rousselier Damage Model for Aluminium Wingbox Aircraft Structure
Numerical Inspection based on Quasi-Static Analysis using Rousselier Damage Model for Aluminium Wingbox Aircraft Structure Open
The present paper illustrates a modelling technique of void damage prediction using constitutive Rousselier damage model in wingbox aircraft structure. The high possibility of aluminium wingbox structure to deform during operating become a…
View article: Analysis on Cracked Commuter Aircraft Wing Under Dynamic Cruise Load By Means of XFEM
Analysis on Cracked Commuter Aircraft Wing Under Dynamic Cruise Load By Means of XFEM Open
In this paper, a new investigation of crack propagation on a commuter aircraft wing is discussed. The aircraft is a 19-seater multi-purpose commuter aircraft designed for a mission on the remote area. The dynamic load acting on the wing is…
View article: Structural integrity assessment of cracked composite plate under aeroelastic loading by means of XFEM
Structural integrity assessment of cracked composite plate under aeroelastic loading by means of XFEM Open
In this paper, a novel procedure to analyse dynamic crack under aeroelastic loading by means of XFEM and Doublet Lattice Method (DLM) - FEM coupling is presented. The present work performed a new investigation on the crack propagation on t…
View article: Evaluation of piezoelectric energy harvester under dynamic bending by means of hybrid mathematical/isogeometric analysis
Evaluation of piezoelectric energy harvester under dynamic bending by means of hybrid mathematical/isogeometric analysis Open
In this paper, a novel hybrid mathematical/isogeometric analysis (IGA) scheme is implemented to evaluate the energy harvesting of the piezoelectric composite plate under dynamic bending. The NURBS-based IGA is applied to obtain the structu…
View article: Characterisation of creep behaviour using the power law model in copper alloy
Characterisation of creep behaviour using the power law model in copper alloy Open
This paper presents a numerical strategy for the characterisation of the creep behaviour
\nmodel of the copper alloy, which is widely used in aircraft applications under creep
\nconditions. The high possibility of the material failing, whi…
View article: An approach for dynamic analysis of stationary cracks using XFEM
An approach for dynamic analysis of stationary cracks using XFEM Open
A numerical implementation of the eXtended Finite Element Method (XFEM) is presented. The proposed approach solves the system of discrete equations using an explicit integration scheme and it is capable of addressing dynamic and static fra…
View article: What triggers a microcrack in printed engineering parts produced by selective laser sintering on the first place?
What triggers a microcrack in printed engineering parts produced by selective laser sintering on the first place? Open
View article: Mixed-mode damage into a CGRP cruciform subjected to biaxial loading
Mixed-mode damage into a CGRP cruciform subjected to biaxial loading Open
In this paper, a three-dimensional progressive damage model (PDM) is implemented within a chopped glass-reinforced polyester (CGRP) cruciform structure for modelling its damage under loading. Three different cruciform specimens subjected t…