PSI - Issue 18
Staroverov Oleg A. et al. / Procedia Structural Integrity 18 (2019) 757–764 Staroverov O.A., Wildemann V.E., Tretyakov M.P., Yankin A.S./ Structural Integrity Procedia 00 (2019) 000–000
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deformation properties of glass-reinforced plastics is typical for samples that have reinforcement angles along the load applied in the structure. As part of the study of the fatigue sensitivity of glass-reinforced plastics with various parameters of cyclic loading, it was found that, for the fiberglass specimens under study, the change in loading parameters maintains the staging of changes in residual static strength. However, variations in impact parameters did not affect the appearance of the curves describing the change in residual rigidity in the process of fatigue accumulation of damage. The influence of the preliminary impact on the deformation properties of carbon-fiber specimens is revealed. Even though the impact reduces the value of the maximum compression load (P, kN) under compression, the length of the equilibrium deformation section is more pronounced. Acknowledgements The work was carried out in the Perm National Research Polytechnic University with support of the Russian Science Foundation (Project 16-19-00069). References Alam, P., Mamalis, D., Robert, C., Floreani, C., Ó Brádaigh, C.M., 2019. The fatigue of carbon fibre reinforced plastics - A review. Composites Part B: Engineering 166, 555–579. Alves, M., Pimenta, S., 2018. A computationally-efficient micromechanical model for the fatigue life of unidirectional composites under tensiontension loading. International Journal of Fatigue 116, 677–690. Barbu, L.G., Oller, S., Martinez, X., Barbat, A.H., 2019. High-cycle fatigue constitutive model and a load-advance strategy for the analysis of unidirectional fiber reinforced composites subjected to longitudinal loads. Composite Structures 220, 622–641. Bey K., Tadjine K., Khelif R., Chemami A., Benamira, M., Azari Z., 2015. Mechanical Behavior of Sandwich Composites Under Three-Point Bending Fatigue // Mechanics of Composite Materials 6, 747–756. Borrelli, Strength. R., Franchitti, S., Di Caprio, F., Mercurio, U., Zallo. A., 2014. A Repair Criterion for Impacted Composite Structures Based on the Prediction of the Residual Compressive Procedia Engineering 88, 117–124. Caminero, M.A., García-Moreno, I., Rodríguez, G.P., 2018. Experimental study of the influence of thickness and ply-stacking sequence on the compression after impact strength of carbon fibre reinforced epoxy laminates. Polymer Testing 66, 360–370. Chen, X., Sun, Y., Wu, Z., Yao, L., Zhang, Y., Zhou, S., Liu, Y., 2019. An investigation on residual strength and failure probability prediction for plain weave composite under random fatigue loading. International Journal of Fatigue 120, 267–282. Degrieck, J., Van Paepegem, W., 2001. Fatigue damage modeling of fibre-reinforced composite materials: Review. Applied Mechanics Reviews 54 (4), 279–300. Deveci, H.A., Artem, H.S., 2018. On the estimation and optimization capabilities of the fatigue life prediction models in composite laminates. Journal of Reinforced Plastics and Composites 37 (21), 1304–1321. Ganesana, C., Joanna, P.S., 2018. Fatigue Life and Residual Strength prediction of GFRP Composites: An Experimental and Theoretical approach. Latin American Journal of Solids and Structures 15(7), e72. 16 Gao, J., An, Z., 2019. A new probability model of residual strength of material based on interference theory. International Journal of Fatigue 118, 202-208. Guillaud, N., Froustey, C., Dau, F., Viot, P., 2015. Impact response of thick composite plates under uniaxial tensile preloading. Composite Structures 121, 172–181. Hack, M., Carrella-Payan, D., Magneville, B., Naito, T., Urushiyama, Y., Yamazaki, W., Yokozeki, T., Van Paepegem, W., 2018. A progressive damage fatigue model for unidirectional laminated composites based on finite element analysis: Theory and practice. Frattura ed Integrita Strutturale 12 (46), 54-61. Heimbs, S., Bergmann, T., Schueler, D., Toso-Pentecôte, N., 2014. High velocity impact on preloaded composite plates. Composite Structures 111, 158–168. Hiremath, C.P., Senthilnathan, K., Naik, N.K., Guha, A., Tewari, A., 2019. Mechanistic model for fiber crack density prediction in cyclically loaded carbon fiber-reinforced polymer during the damage initiation phase. Journal of Composite Materials 53 (8), 993–1004. Huang, J., Pastor, M.L., Garnier, C., Gong, X.J., 2019. A new model for fatigue life prediction based on infrared thermography and degradation process for CFRP composite laminates. International Journal of Fatigue 120, 87–95. Hwang, W., Han, K.S., 1986. Cumulative Damage Models and Multi-Stress Fatigue Life Prediction. Journal of Composite Materials 20 (2), 125 153. Kaminski M., Laurin F., Maire F.J., Rakotoarisoa C., Hemon E., 2015. Fatigue damage modeling of composite structures: the ONERA viewpoint. AerospaceLab. June 2015, 1–12. Katunin A., 2018. Criticality of the self-heating effect in polymers and polymer matrix composites during fatigue, and their application in non destructive testing. Polymers 11 (1). Kawai, M., Ishizuka, Y., 2018. Fatigue life of woven fabric carbon/epoxy laminates under alternating R-ratio loading along non-proportional path in the σm-σa plane. International Journal of Fatigue 112, 36–51. Khay, M., Ngo, A.D., Ganesan, R., 2018. Experimental investigation and phenomenological modeling of hygrothermal effect on tensile fatigue behavior of carbon/epoxy plain weave laminates. Journal of Composite Materials 52 (27), 3803–3818. Lemanle Sanga, R.P., Garnier, C., Pantalé, O., 2018. Approaches to simulate impact damages on aeronautical composite structures. AIP Conf. Proc., 030024-1–030024-11. DOI: 10.1063/1.5024174. Lopresto, V., Langella, A., Papa, I., 2016. Residual Strength evaluation after impact tests in extreme conditions on CFRP laminates. Procedia
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