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MODELLING AND EXPERIMENTAL TESTING OF HYBRID JOINTS MADE OF: ALUMINIUM ADHERENDS, ADHESIVE LAYERS AND RIVETS FOR AEROSPACE APPLICATIONS.

Authors : SADOWSKI, T.¹ ; GOLEWSKI, P.¹

Source: Archives of Metallurgy & Materials. Sep2017, Vol. 62 Issue 3, p1577-1583. 7p.

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SKIN-SPAR FAILURE DETECTION OF A COMPOSITE WINGLET USING FBG SENSORS.

Authors : CIMINELLO, MONICA¹ ; DE FENZA1, ANGELO^2,3; DIMINO1, IGNAZIO¹

Source: Archive of Mechanical Engineering. Sep2017, Vol. 64 Issue 3, p287-300. 14p.

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NUMERICAL MODELLING OF A PIEZO ROOF HARVESTING SYSTEM: THE RIGHT COMPONENT SELECTION.

Authors : DI LEO, ROMEO¹ ; VISCARDI, MASSIMO¹ ; TUCCINARDI, FRANCESCO PAOLO²

Source: Archive of Mechanical Engineering. Jun2017, Vol. 64 Issue 2, p257-282. 26p.

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IMPLEMENTATION OF AN ELECTRONIC CIRCUIT FOR SSSA CONTROL APPROACH OF A PLATE TYPE ELEMENT AND EXPERIMENTAL MATCH WITH A FEED-FORWARD APPROACH.

Authors : VISCARDI, MASSIMO¹ ; DI LEO, ROMEO¹

Source: Archive of Mechanical Engineering. Dec2016, Vol. 63 Issue 4, p665-677. 13p.

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Performances' Estimation by Tests of Composite Material Structures With Respect to the Lay-Up Configuration and Mixing the Position of Tape and Fabric Laminae.

Authors : Di Leo, R.¹; De Fenza, A.¹; Barile, M.¹

Source: Archive of Mechanical Engineering. Dec2015, Vol. 62 Issue 4, p553-564. 12p.

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Drop Test Simulation for An Aircraft Landing Gear Via Multi-Body Approach.

Authors : Leo, Romeo Di; Fenza, Angelo De¹; Barile, Marco¹

Source: Archive of Mechanical Engineering. 2014, Vol. 61 Issue 2, p287-304. 18p.

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MODELLING AND EXPERIMENTAL TESTING OF HYBRID JOINTS MADE OF: ALUMINIUM ADHERENDS, ADHESIVE LAYERS AND RIVETS FOR AEROSPACE APPLICATIONS.

SKIN-SPAR FAILURE DETECTION OF A COMPOSITE WINGLET USING FBG SENSORS.

NUMERICAL MODELLING OF A PIEZO ROOF HARVESTING SYSTEM: THE RIGHT COMPONENT SELECTION.

IMPLEMENTATION OF AN ELECTRONIC CIRCUIT FOR SSSA CONTROL APPROACH OF A PLATE TYPE ELEMENT AND EXPERIMENTAL MATCH WITH A FEED-FORWARD APPROACH.

Performances' Estimation by Tests of Composite Material Structures With Respect to the Lay-Up Configuration and Mixing the Position of Tape and Fabric Laminae.

Drop Test Simulation for An Aircraft Landing Gear Via Multi-Body Approach.

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