2019
DOI: 10.3390/app9112372
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Numerical–Experimental Correlation of Impact-Induced Damages in CFRP Laminates

Abstract: Composite laminates are characterized by high mechanical in-plane properties and poor out-of-plane characteristics. This issue becomes even more relevant when dealing with impact phenomena occurring in the transverse direction. In aeronautics, Low Velocity Impacts (LVIs) may occur during the service life of the aircraft. LVI may produce damage inside the laminate, which are not easily detectable and can seriously degrade the mechanical properties of the structure. In this paper, a numerical-experimental invest… Show more

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Cited by 36 publications
(23 citation statements)
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References 36 publications
(53 reference statements)
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“…The FRP composites are essentially brittle with no plastic deformation, thus adequately described using a bilinear stress-strain curves with elastic and softening responses. The softening response represents the permanent deformation of the material, described through the continuous degradation of stiffness and strength to complete fracture [10][11][12][13]. The general loading on composite structures, including axial, flexural, and torsional loads, generates a complex stress state in the material.…”
Section: Introductionmentioning
confidence: 99%
“…The FRP composites are essentially brittle with no plastic deformation, thus adequately described using a bilinear stress-strain curves with elastic and softening responses. The softening response represents the permanent deformation of the material, described through the continuous degradation of stiffness and strength to complete fracture [10][11][12][13]. The general loading on composite structures, including axial, flexural, and torsional loads, generates a complex stress state in the material.…”
Section: Introductionmentioning
confidence: 99%
“…They concluded that it is possible to predict the Mode II interlaminar fracture toughness by using the formula where B is a coefficient that takes into account the additional shear stress contribution. Considering the loading conditions found in impact events, the main cause of failure within the composite structure can be related to the shear stress [ 41 , 42 , 43 ] localised within a structure during the dynamic loading. Consequently, it is possible to assume that Mode II failure is dominant and high dependency from the ply angle is expected for the G c value in this loading condition.…”
Section: Functionally Graded Pitch (Fgp) Laminatesmentioning
confidence: 99%
“…Concrete material is also investigated in relation to impact resistance [18] and self-healing properties [19]. Impact behavior is studied with reference to laminate composites [20,21]. Other papers devoted to rocks concern their cutting resistance [22] and their multiaxial response under dry and saturated conditions [23].…”
Section: Fracturementioning
confidence: 99%