2011
DOI: 10.1016/j.compstruct.2011.04.029
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On the response of two commercially-important CFRP structures to multiple ice impacts

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Cited by 78 publications
(31 citation statements)
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“…5a). Although these events have a low probability (less than 1 m −2 yr −1 ), they may thus be sufficient to cause damage to blade coatings in isolation from the effects of the cumulative fatigue (Appleby- Thomas et al, 2011;Kim and Kedward, 2000). Conversely, individual rain impacts rarely exceed 5.2 J at any site.…”
Section: Station Codementioning
confidence: 99%
See 1 more Smart Citation
“…5a). Although these events have a low probability (less than 1 m −2 yr −1 ), they may thus be sufficient to cause damage to blade coatings in isolation from the effects of the cumulative fatigue (Appleby- Thomas et al, 2011;Kim and Kedward, 2000). Conversely, individual rain impacts rarely exceed 5.2 J at any site.…”
Section: Station Codementioning
confidence: 99%
“…The stress induced by individual high net collision impacts with hydrometeors may, in principle, exceed the strength of the material. Estimates of the failure energy threshold of a composite structure vary widely (e.g., values of 72-140 J are given in Appleby- Thomas et al, 2011) and may exceed 300 J for leading-edge thicknesses and hailstone diameters > 20 mm (Kim and Kedward, 2000). However, conceptually the erosion of homogeneous materials is most frequently considered using a three-stage model.…”
Section: Introduction and Objectivesmentioning
confidence: 99%
“…More recently Carney et al [20] performed high velocity impacts of ice cylinders on load cell in order to generate experimental data to validate an ice material model; the contact force was not quantified although it is distinguished from the load cell measurement. ApplebyThomas et al [22] studied the effect of multiple impacts on carbon/epoxy composite panels; Combescure et al [23] analysed the high velocity impact of cylindrical ice on both rigid and flexible targets. Hong et al [24] focused its investigation in the impact of very small particles of ice on carbon/epoxy composite laminates.…”
Section: Introductionmentioning
confidence: 99%
“…The SHEAR -a material is failed as shift, the SPALL -a material is failed as a separation, MELTING -internal energy more than energy of fusion, P GAS -internal energy of a material more than energy of sublimation, GAS -the substance is evaporated. Elimination of the evaporated fragments allows simplifying the analysis of a problem [11][12][13][14][15][16][17][18][19][20][21][22]. The areas of light grey color indicate material fusion and the dark areas correspond to a material condition, while its internal energy more than sublimation energy.…”
Section: Problem Statement the Initial Data And Analysis Resultsmentioning
confidence: 99%