2018
DOI: 10.1016/j.compstruct.2018.02.057
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An investigation of in-plane dynamic behavior of adhesively-bonded composite joints under dynamic compression at high strain rate

Abstract: This study examines the behaviour of adhesively-bonded composite joints under dynamic compression tests. The purpose of this work is to use the split Hopkinson pressure bar (SHPB) for the dynamic characterization of adhesively bonded joints subjected to in-plane compression loading and in particular, the effect of strain rate on the mechanical behaviour and the damage kinetics. These joints are studied using glass/vinylester composite materials which are frequently used in naval applications Compression tests … Show more

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Cited by 38 publications
(24 citation statements)
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“…32 During our test campaign carried out with Hopkinson bars, we always make sure to verify the various validation hypotheses, see our various papers on the subject in particular. 33,34 Figure 4 shows that the equilibrium condition is well verified. Table 5 presents the standard deviation and the mean value.…”
Section: Shpb Test Techniquementioning
confidence: 74%
“…32 During our test campaign carried out with Hopkinson bars, we always make sure to verify the various validation hypotheses, see our various papers on the subject in particular. 33,34 Figure 4 shows that the equilibrium condition is well verified. Table 5 presents the standard deviation and the mean value.…”
Section: Shpb Test Techniquementioning
confidence: 74%
“…For the case of the vertical temperature profiles (Figure 12(a), (c) and (e)), one can observe a higher temperature at the incident and transmitted/specimen interfaces than that at the adhesive layer and this may be caused by either crushing/delamination of external layer or by friction effects at these strain rates. However, previous work 21,2531 have proved that the friction effects are negligible under dynamic compressive tests using SHPB and the damage is caused only by the multiplication of the microscopic and macroscopic damage modes. Thus, the heating at the interfaces seems to be a result only of global matrix failure and not of friction effects.…”
Section: Damage Kineticsmentioning
confidence: 93%
“…Due to the excellent peel resistance and impact strength, these adhesive layers can be applied to structures such as in automobiles and wind turbines (e.g., to join composite blades to metal hubs). The dynamic performance of the structure can play a crucial role in these applications. Determining the high strain rate response of such structural adhesives requires not only the reliable experimental characterization but also the quantitative constitutive prediction.…”
Section: Introductionmentioning
confidence: 99%