Failure Criteria for FRP Laminates
By C. Dávila, Pedro P. Camanho, C. Rose. 2005
554 citations recorded by the source corpus.
Subfields: Building and Construction, Mechanical Engineering, Mechanics of Materials
View Paper: https://www.semanticscholar.org/paper/48ca72ee8ff6266215cd87030ee1cecd2bd046fc
How researchers see this paper
The researchers whose trusted networks rank it highest, strongest advocate first. Every researcher gets a different order.
In Building and Construction
- Pedro P. Camanho
- F. P. van der Meer
- Lambertus J. Sluys
- Javier Llorca
- Carlos Gonz'alez
- G. Catalanotti
- A. Melro
- S. Pinho
In Mechanical Engineering
- Pedro P. Camanho
- G. Catalanotti
- C. Dávila
- Carlos Gonz'alez
- P. Maimí
- F. P. van der Meer
- Lambertus J. Sluys
- Javier Llorca
In Mechanics of Materials
- Pedro P. Camanho
- F. P. van der Meer
- Lambertus J. Sluys
- G. Catalanotti
- Carlos Gonz'alez
- Cláudio S. Lopes
- S. Hallett
- C. Dávila
Citations in the corpus
- Computational micromechanics of the transverse and shear behavior of unidirectional fiber reinforced polymers including environmental effects (2017, background): “there is a need to improve existing ply failure criteria that rely only on ply properties [8, 9].”
- Measurement of resistance curves in the longitudinal failure of composites using digital image correlation (2010, unknown): “Despite the significant advances in the analysis models for the prediction of fracture in composite materials such as advanced failure criteria and associated damage models [1–7], sophisticated kinematic representations of failure mechanisms [8,9], and cohesive elements to deal with delamination [10”
- Hybrid titanium–CFRP laminates for high-performance bolted joints (2009, background): “However, the shear stresses do play an important 212 role in fibre kinking [24] and their absence in the failure criteria results in an over-prediction of 213 the elastic limit.”
- Computational modeling of complex failure mechanisms in laminates (2012, background): “A possible future extension of the model is to use a more advanced damage evolution law, taking into account measurements on the increasing fracture toughness with increasing crack length (the so-called R curve), such as has been proposed by Dávila et al.70 This would allow for a better representat”
- Failure locus of fiber-reinforced composites under transverse compression and out-of-plane shear (2008, methodology): “The failure condition in Puck and LaRC criteria is given by the Mohr–Coulomb model according to [20],”
- Design optimization and manufacture of hybrid glass/carbon fiber reinforced composite bumper beam for automobile vehicle (2015, background): “It had been reported that the transverse strengths almost depend on the mechanical properties of matrix [11, 12].”
- Three-dimensional failure criteria for fiber-reinforced laminates (2013, methodology): “In the region characterized by kinking for matrix compression, the LaRC03 failure criterion predicts an increase of the apparent axial compressive strength and this is confirmed by experimental results [23].”
- A design methodology for mechanically fastened joints in laminated composite materials (2006, methodology): “The parameter g is the coefficient of longitudinal influence defined in [17,18]:”
- Mesh‐independent matrix cracking and delamination modeling in laminated composites (2011, methodology): “In the present paper, the LaRC03 failure criterion [28] is used.”
- Prediction of in situ strengths and matrix cracking in composites under transverse tension and in-plane shear (2006, background): “As a result of that effort, a set of six criteria for predicting failure of unidirectional FRP laminates were proposed [19], [20].”
- A phantom node formulation with mixed mode cohesive law for splitting in laminates (2009, methodology): “For failure inside the ply, numerous formulations have been proposed for stress based failure criteria, ranging from classical criteria by Tsai and Wu (1971) and Hashin (1980) to more recent ones by Puck and Schürmann (1998, 2002) and Dávila et al. (2005). These strength criteria can be used in prog”