Damage in CFRPs due to low velocity impact at low temperature

By T. G. Rı́o, Ramón Zaera, E. Barbero, Carlos Navarro. 2005

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Low velocity impact behavior of interlayer hybrid composite laminates with carbon/glass/basalt fibres (2019, methodology): “To simulate the real loading conditions, multiple factors have been considered including temperature [12], repeated impact [13] and coupling cases [14, 15].”
Properties of cryogenic and low temperature composite materials – A review (2020, background): “Epoxy (8552) CF (AS4) Woven 123 Eabs↓ (low impact energy) ↑ (high impact energy) [184] VE CF UD 173 Eabs↑130% [56] VE CF Woven 223 Eabs↓ [71] VE (510A) CF (T700) Woven 223 Eabs↓ (low impact energy) ↑ (high impact energy) [195] Thermoset resin – Glass fibre Epoxy GF Woven 223 Eabs↓3% (low impact ener”
Low-velocity impact response of woven Kevlar/epoxy laminated composites reinforced with multi-walled carbon nanotubes at ambient and low temperatures (2014, background): “[11].”
A comparison of multi-scale 3D X-ray tomographic inspection techniques for assessing carbon fibre composite impact damage (2013, background): “To achieve very high levels of detail to study the material microstructure, traditional materialographic sectioning followed by microscopy can be performed [7, 8].”