George Labeas

Prof. Dr. George Labeas

Department of Mechanical Engineering and Aeronautics, University of Patras, 26504 Rio, Greece
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Research Focus & Metrics

Academic Career Length

22Years (2005-Present)

(Calculated once Scilit publication data is synced: current year − year of first publication + 1)

Representative Publications

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28 May 2012 in Journal of Sandwich Structures & Materials
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EPEvangelos Ptochos
Evangelos Ptochos
GLGeorge Labeas
George Labeas
The mechanical properties of micro-lattice structures made of interconnected metallic struts are calculated analytically, in order to derive their elastic modulus and Poisson’s ratio in the three Cartesian directions. The geometry of the investigated unit cell is a body centered cuboid, which is a more generic case of the well-known body centered cubic geometry. The Bernoulli–Euler and Timoshenko beam theories are used for the analytical solution of the unit cell response under complex loading. The derived elastic constants are compared to the relative numerical ones. The influence of geometrical parameters on the stiffness coefficients of the cellular structure is parametrically determined. The derived elasticity matrices are introduced in a homogenised numerical model of the core and its results are compared to a numerical model with explicit representation of the core geometry indicating an excellent accuracy, while the solution time is considerably reduced.

1 November 2005 in Applied Composite Materials
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TKTh. Kermanidis
Th. Kermanidis
GLGeorge Labeas
George Labeas
MSM. Sunaric
M. Sunaric
LUL. Ubels
L. Ubels

6 May 2011 in International Journal of Damage Mechanics
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Journal Article
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GLGeorge Labeas
George Labeas
SBS. D. Belesis
S. D. Belesis
IDI. Diamantakos
I. Diamantakos
KTK. I. Tserpes
K. I. Tserpes
Progressive damage modeling (PDM) is a well-established methodology for the prediction of damage initiation and evolution in composite structures. However, as conventional PDM methodology involves a large post-processing procedure, it is impractical for application in large-scale structures due to the high computational cost it requires. In this study, the local character of nonlinearity, due to the scale of the damage topology compared to the size of the entire structure, is exploited to propose proper modifications in the ‘classical’ PDM methodology. Specifically, the sub-modeling technique principles are combined and integrated in the PDM methodology and the appropriate modifications required are discussed. Furthermore, two damage prediction indices, which are related to the criticality of damage state at specific sub-areas (material layers) of the structure are introduced, in order to achieve significant reductions of the required computational time. Both the improvements make the application of PDM in large-scale composite structures practically feasible; this is demonstrated in the case of a generic composite shear joint whose numerical model comprises over a million degrees of freedom.

1 February 2010 in Science and Technology of Welding and Joining
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GMG. A. Moraitis
G. A. Moraitis
GLGeorge Labeas
George Labeas
An innovative methodology for the semi-analytical calculation of the total heat generated during the friction stir welding (FSW) process is proposed. The methodology includes a simple and straightforward procedure for the determination of the heat produced due to the material stirring, combines the advantages of the conventional moving heat approach with those of alternative modelling approaches, (i.e. computational fluid dynamics or arbitrary Lagrangian Eulerian), while, simultaneously, overcomes some of their main limitations. Moreover, the predicted FSW heat energy is introduced in a global three-dimensional finite element thermal model, which predicts the spatial temperature history developing in the welded parts during the process. The overall methodology is validated through experimental temperature measurements. Finally, the global thermal model results are introduced in a thermomechanical model, from which the residual stress and distortion fields are predicted. The proposed methodology can be easily modified and used in FSW applications of variable welded plate geometry, FSW tool type, joint type and process parameters.

27 February 2023 in Alloys
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HPHarry Psihoyos
Harry Psihoyos
GLGeorge Labeas
George Labeas
One of the main challenges encountered in the Laser-based Powder Bed Fusion (L-PBF) Additive Manufacturing (AM) process is the fabrication of defect-free parts. The presence of defects severely degrades the mechanical performance of AM parts and especially their fatigue strength. The most popular and reliable method to assess the ability of the employed process parameters for the fabrication of full-density parts is the process windows map, also known as printability map. However, the experimental procedure for the design of the printability maps and the identification of the optimum-density process parameters is usually time-consuming and expensive. In the present work, a modelling framework is presented for the determination of a printability map and the optimization of the L-PBF process based on the prediction and characterization of melt-pool geometric features and the prediction of porosity of small samples of 316L SS and Ti-6Al-4V metal alloys. The results are compared with available experimental data and present a good correlation, verifying the modelling methodology. The suitability of the employed defect criteria for each material and the effect of the hatch-spacing process parameter on the optimum-density parameters are also presented.