An experimental investigation of the impact response of composite laminates
By M. Aktaş, C. Atas, B. M. Içten, R. Karakuzu. 2009
261 citations recorded by the source corpus.
Subfields: Mechanical Engineering, Mechanics of Materials, Polymers and Plastics
View Paper: https://www.semanticscholar.org/paper/b72913931061c5027e649e68ec9492bd946096a1
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In Mechanical Engineering
In Mechanics of Materials
In Polymers and Plastics
Citations in the corpus
- Low-velocity impact and residual tensile strength analysis to carbon fiber composite laminates (2010, background): “These damages cause reduction in structural stiffness and strength, leading to growth of the damage and final fracture [23, 24 ].”
- Impact damage on fibre-reinforced polymer matrix composite – A review (2014, background): “Aktas et al.99 presented a schematic illustration for different damage modes in composite laminates, as shown in Figure 4.”
- Experimental and numerical studies on the impact response of damage-tolerant hybrid unidirectional/woven carbon-fibre reinforced composite laminates (2018, unknown): “Mehmet et al. [11] investigated the impact response of cross-ply and angle-ply glass/epoxy laminates under different impact energy levels.”
- Glass fiber-reinforced polymer composites – a review (2014, methodology): “Aktas et al.45 investigated compression after impact (CAI) behaviour of unidirectional E-GF-reinforced epoxy matrix composite subjected to low-velocity impact energy for various temperatures such as 40 C, 60 C, 80 C and 100 C.”
- Influence of matrix toughness and ductility on the compression-after-impact behavior of woven-ply thermoplastic- and thermosetting-composites: A comparative study (2014, background): “resistance to buckling of the sub-laminates rather than their inplace resistance [8,14,15].”
- Impact and after-impact properties of carbon fibre reinforced composites enhanced with multi-wall carbon nanotubes (2010, methodology): “With the impact and the absorbed energies available, the energy profile diagram [27,28] was produced and it is presented in Fig.”