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		题名	作者	年代	出处	被引量
	1	Numerical evaluation of aerodynamic and inertial contributions to Darrieus wind turbine blade deformation显示文摘	MARCO RACITI CASTELLI ANDREA DAL MONTE MARINO QUARESIMIN		0，，：	1
	2	Fatigue behaviour and life assessment of composite laminates under multiaxial loadings 显示文摘	MARINO Quaresimin LUCA Susmel RAMESH Talreja	2010	International Journal of Fatigue2010，32，1：	1
	3	Numerical evaluation of aerodynamic and inertial contributions to Darrieus wind turbine blade deformation 显示文摘	Raciti Castelli M Dal Monte A Quaresimin M	2013	Renewable Energy2013，51，：	1
	4	Glass-fibre-reinforced composites with enhanced mechanical and electrical properties – Benefits and limitations of a nanoparticle modified matrix显示文摘	Malte H.G. Wichmann Jan Sumfleth Florian H. Gojny Marino Quaresimin Bodo Fiedler Karl Schulte	2006	Engineering Fracture Mechanics2006，，16：	1
	5	Multiaxial fatigue behaviour of a severely notched earbonsteel 显示文摘	Atzori B Berto F Lazzarin P Quaresimin M	2006	International Journal of Fatigue2006，28，：	1
	6	Fatigue behaviour and damage evolution of single lap bonded joints in composite material 显示文摘	Quaresimin M Ricotta M	2006	Compos Sci Technol2006，66，2：	1
	7	Stress intensity factors and strain energy release rates in single lap bonded joints in composite materials 显示文摘	Quaresimin M Ricotta M	2006	Composites Science and Technology2006，56，5：	1
	8	Energy absorption in composite laminates under impact loading显示文摘	Quaresimin M Ricotta M Martello L	2013	Composites Part B: Engineering2013，44，44：	1
	9	Two--stage Fatigue Loading of Woven Carbon Fiber Reinforced Laminates显示文摘	Found M S Quaresimin M	2003	Fatigue & Fracture Engineering Materials & Structures2003，26，：	1
	10	MIXED MODES INTERLAMINAR FRACTURE TOUGHNESS OF CFRP LAMINATES TOUGHENED WITH CNF INTERLAYER显示文摘In the present paper, the influence of carbon nanofiber on interlaminar fracture toughness of CFRP investigated using MMB(Mixed Mode Bending) tests. Vapor grown carbon fiber VGCF and VGCF-S, and multi-walled carbon nanotube MWNT-7 has been employed for the toughener of the interlayer on the CFRP laminates. In order to evaluate the fracture toughness and mixed mode ratio of it, double cantilever beam (DCB) tests, end notched fracture (ENF) tests and mixed mode bending (MMB) tests have been carried out. Boundary element analysis was applied to the CFRP model to compute the interlaminar fracture toughness, where extrapolation method was used to determine the fracture toughness and mixed mode ratio. The interlaminar fracture toughness and mixed mode ratio can be extrapolated by stress distribution in the vicinity of the crack tip of the CFRP laminate. It was found that the interlaminar fracture toughness of the CFRP laminates was improved inserting the interlayer made by carbon nanofiber especially in the region where shear mode deformation is dominant.	Masahiro Arai Tatsuya Sasaki Satoshi Hirota Hiroaki Ito Ning Hu Marino Quaresimin	2012	Acta Mechanica Solida Sinica2012，25，3：	0

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