LAZZERI, LUIGI Statistiche

LAZZERI, LUIGI  

DIPARTIMENTO DI INGEGNERIA CIVILE E INDUSTRIALE  

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Titolo Data di pubblicazione Autore(i) File
Assessment of a numerical strategy for fatigue growth and shape evolution of a corner crack from a pin-loaded hole 1-gen-2021 Bovecchi, F.; Boni, L.; Fanteria, D.; Lazzeri, L.
Numerical simulation of fatigue crack growth in an open-hole specimen 1-gen-2021 Bovecchi, F.; Santangelo, M.; Boni, L.; Fanteria, D.; Lazzeri, L.
Fatigue crack growth in pin-loaded cold-worked holes 1-gen-2019 Boni, L.; Fanteria, D.; Furfari, D.; Lazzeri, L.
Influence of environment conditioning on the interlaminar fracture toughness of a graphite/epoxy unidirectional material 1-gen-2018 Boni, L.; Fanteria, D.; Lazzeri, L.; Panettieri, E.; Rigamonti, M.; Mariani, U.
Experimental characterization of the interlaminar fracture toughness of a woven and a unidirectional carbon/epoxy composite 1-gen-2017 Fanteria, Daniele; Lazzeri, Luigi; Panettieri, Enrico; Mariani, U.; Rigamonti, M.
Numerical prediction of fatigue crack propagation in Cold-Expanded Holes 1-gen-2017 Boni, Luisa; Fanteria, Daniele; Lazzeri, Luigi; Furfari, Domenico
Predicting fatigue crack growth emanating from cold-expanded holes 1-gen-2015 Lazzeri, Luigi; Furfari, Domenico; Fu, Qiang; Wetzel, Anja; Biasizzo, Mauro Bruno; Busse, David Osman
Crack propagation in flat panels stiffened by bonded pads 1-gen-2014 Boni, Luisa; Fanteria, Daniele; Lanciotti, Agostino; Lazzeri, Luigi; Palmiero, F.; Sollo, A.
Improved methodology for the design of damage tolerant helicopter structures in composite materials 1-gen-2013 Airoldi, A.; Baldi, A.; Coiro, M.; Fanteria, Daniele; Lazzeri, Luigi; Mariani, U.; Rigamonti, M.; Sala, G.; Scapinello, F.
Methods for design and health monitoring of damage tolerant helicopter structures in fiber-reinforced polymer composites 1-gen-2013 Baldi, A.; Airoldi, A.; Bettini, P.; Fanteria, Daniele; Lazzeri, Luigi; Mariani, U.; Sala, G.; Scapinello, F.
Fatigue crack growth in stiffened panels,integrally machined or welded (LBW or FSW): the DaToN project common testing program 1-gen-2011 Lanciotti, Agostino; Lazzeri, Luigi; C., Polese; C., Rodopoulos; P., Moreira; A., Brot; G., Wang; L., Velterop; G. BIALLAS AND J., Klement
Application of damage tolerance principles to the design of helicopters 1-gen-2009 Lazzeri, Luigi; U., Mariani
Experimental Tests and Numerical Analyses of Fibre Metal Laminates Panels Under Shear Load with Bonded Window Frame 1-gen-2009 Boni, Luisa; Lanciotti, Agostino; Lazzeri, Luigi
FATIGUE RESISTANCE AND RESIDUAL STRENGTH OF RIVETED JOINTS IN FML 1-gen-2009 Lanciotti, Agostino; Lazzeri, Luigi
Fatigue resistance and residual strength of riveted joints in FML Fatigue and Fracture of Engineering Materials and Structures. Vol. 32, 2009, pp. 837-846. Luglio 2009 1-gen-2009 Lanciotti, Agostino; Lazzeri, Luigi
Durability and Damage Tolerance of Aircraft Structures: Metals vs. Composites 1-gen-2008 Lazzeri, Luigi; Salvetti, Attilio
Dimensionamento a fatica di elementi strutturali di elicottero 1-gen-2003 Catalini, A.; Lazzeri, Luigi
Fatigue crack propagation in thin 2024 sheets under typical helicopter spectra 1-gen-2002 Lazzeri, Luigi; Ratti, G.
Fatigue behaviour of riveted Glare lap joints 1-gen-2001 Lazzeri, Luigi
Fatigue Problems in the Design of Fuselage Panels in Glare 1-gen-2001 Cavallini, Giorgio; Galatolo, Roberto; Lazzeri, Luigi