Search Results - "Armentani, E."

Correlation between real geometry and tensile mechanical behaviour for Ti6Al4V electron beam melted thin specimens by Sepe, R., Franchitti, S., Borrelli, R., Di Caprio, F., Armentani, E., Caputo, F.

“…•Surface morphology and tensile properties are affected by the specimen size.•Measured and effective areas difference decreases as the specimen thickness…”
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FML full scale aeronautic panel under multiaxial fatigue: Experimental test and DBEM Simulation by Armentani, E., Citarella, R., Sepe, R.

“…This paper concerns the numerical and experimental characterization of the static and fatigue strength of a flat stiffened panel, designed as a Fibre Metal…”
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Stress corrosion cracking behaviour of conventional and innovative aluminium alloys for aeronautic applications by Astarita, A., Bitondo, C., Squillace, A., Armentani, E., Bellucci, F.

“…In this work, the stress corrosion cracking (SCC) behaviour of both innovative and conventional friction stir welded aluminium alloys was investigated. Similar…”
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Numerical and Experimental Investigation on the Structural Behaviour of a Horizontal Stabilizer under Critical Aerodynamic Loading Conditions by Armentani, E., De Luca, A., Citarella, R., Sepe, Raffaele

“…The aim of the proposed research activity is to investigate the mechanical behaviour of a part of aerospace horizontal stabilizer, made of composite materials…”
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Established Numerical Techniques for the Structural Analysis of a Regional Aircraft Landing Gear by Armentani, E., Apicella, A., Marro, A., Greco, A., De Luca, A., Caputo, Francesco, Sepe, Raffaele

“…Usually during the design of landing gear, simplified Finite Element (FE) models, based on one-dimensional finite elements (stick model), are used to…”
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DBEM and FEM analysis on non-linear multiple crack propagation in an aeronautic doubler-skin assembly by Armentani, E., Citarella, R.

“…The performance of a riveted patch repair, applied on a cracked panel, is simulated by using both a commercially available boundary element code (BEASY) and a…”
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Evaluation of energy release rate for delamination defects at the skin/stringer interface of a stiffened composite panel by Armentani, E., Caputo, F., Esposito, R., Godono, G.

“…This paper deals with numerical investigation on a stiffened composite panel under longitudinal compression load, in presence of artificial delamination…”
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Neural networks for fatigue crack propagation predictions in real-time under uncertainty by Giannella, V., Bardozzo, F., Postiglione, A., Tagliaferri, R., Sepe, R., Armentani, E.

“…•Residual fatigue life prediction models are created by using neural networks.•FEM and Monte Carlo methods are used to generate data to train the neural…”
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Numerical investigation on the fracture failure of a railway axle by Giannella, V., Sepe, R., Borrelli, A., De Michele, G., Armentani, E.

“…•An investigation on the failure of a railway axle is presented.•Crack-growth propagation was simulated by using two numerical codes.•A loading spectrum and a…”
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Experimental and FEM numerical assessment of multiaxial fatigue failure criteria for a rolling Stock's seats structure by Sepe, R., Greco, A., De Luca, A., Armentani, E., Berto, F.

“…This paper deals with the experimental and numerical investigations of the structural behaviour of a rolling stock's seats system under static and fatigue…”
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FML full scale aeronautic panel under multiaxial fatigue: Experimental test and DBEM Simulation: Multiaxial Fracture by ARMENTANI, E, CITARELLA, R, SEPE, R

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