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Sadighi, M. (author), Alderliesten, R.C. (author)
A review of experimental evidence from the literature in relation to “impact fatigue”, “multiple impacts”, and “repeated impacts” on FRP composites, along with articles discussing theoretical and numerical simulations, is provided. A new terminology and definition is presented to clear the meanings of these types of loadings. Experimental...
review 2022
document
Sadighi, M. (author), Pärnänen, T. (author), Alderliesten, R.C. (author), Sayeaftabi, M. (author), Benedictus, R. (author)
The impact response of fiber metal laminates (FMLs), has been investigated with experiments and numerical simulations, which is reported in this article. Low-velocity impacts were carried out to study the effects of metal type and thickness within FMLs. Glare5-3/2 laminates with two aluminum layer thicknesses and a similar FML containing...
journal article 2012
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Huo, L. (author), Alderliesten, R.C. (author), Sadighi, Mojtaba (author)
To further investigate the effects of in-plane and out-of-plane stresses on the delamination initiation for composite laminates under out-of-plane loading, this paper reports a joint experimental and numerical study, in which the fully clamped rectangular CFRP composite laminates were subjected to out-of-plane quasi-static indentations. The...
journal article 2022
document
Ji, C. (author), Hu, Jiqiang (author), Sadighi, M. (author), Alderliesten, R.C. (author), Wang, Bing (author), Sun, Yuguo (author)
Fiber metal laminates (FMLs) provide a reliable approach for achieving lightweight in high-speed aerospace vehicles. However, the weak interfacial properties between metals and composites could significantly affect the deformation and failure modes of FMLs. In this paper, the low-velocity impact responses and damage mechanisms of CF/PEEK-Ti...
journal article 2022
document
Sadighi, M. (author), Alderliesten, R.C. (author), Fathi, Azadeh (author), Soltannia‬, Babak (author), Hedayati, R. (author)
Damages to aircraft fuselages by ice impactors are categorized as barely visible impact damage (BVID). As the application of composite laminates in manufacturing aircraft fuselage is increasing rapidly, studying hail impact on composite laminates seems crucial. Investigation of variation of delamination area and link-up area for different...
journal article 2023
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