Pub Date : 2025-07-01Epub Date: 2025-05-08DOI: 10.1016/j.jcomc.2025.100608
J.R. Pothnis , A. Hejjaji , G.S. Bhatia , A. Comer
This experimental study investigates the fracture and failure mechanisms of glass fiber reinforced polymer matrix composites fabricated using an in-situ polymerizable thermoplastic and a bio-based epoxy matrix subjected to tension-tension fatigue loading. For both material systems, fatigue tests resulted in linear S-N curves for the 0°, 90° and Quasi-Isotropic (QI) laminates and non-linear (power law) S-N curves for the ±45° and ±30° laminate configurations. However, the main focus of the study was on the failure mechanisms for both the low-cycle and high-cycle fatigue loading regimes. At the macro level, the effect of the different matrices on the characteristic failure mode was generally minimal with all lay-ups exhibiting distributed damage throughout the gauge region except for the 90° laminates where damage was highly localised. However, micro level analysis conducted using SEM and elemental composition analysis revealed significantly different failure mechanisms in the vicinity of the fibre matrix interface for the bio-epoxy (interfacial) and the thermoplastic (cohesive). Overall, both matrices show promise in terms of fatigue performance under benign laboratory conditions and as a stepping stone towards achieving more sustainable matrix options for offshore renewable energy structures in the future.
{"title":"Failure analysis under fatigue loading of glass fibre reinforced in-situ polymerizable thermoplastic and Bio-epoxy based Composites","authors":"J.R. Pothnis , A. Hejjaji , G.S. Bhatia , A. Comer","doi":"10.1016/j.jcomc.2025.100608","DOIUrl":"10.1016/j.jcomc.2025.100608","url":null,"abstract":"<div><div>This experimental study investigates the fracture and failure mechanisms of glass fiber reinforced polymer matrix composites fabricated using an in-situ polymerizable thermoplastic and a bio-based epoxy matrix subjected to tension-tension fatigue loading. For both material systems, fatigue tests resulted in linear S-N curves for the 0°, 90° and Quasi-Isotropic (QI) laminates and non-linear (power law) S-N curves for the ±45° and ±30° laminate configurations. However, the main focus of the study was on the failure mechanisms for both the low-cycle and high-cycle fatigue loading regimes. At the macro level, the effect of the different matrices on the characteristic failure mode was generally minimal with all lay-ups exhibiting distributed damage throughout the gauge region except for the 90° laminates where damage was highly localised. However, micro level analysis conducted using SEM and elemental composition analysis revealed significantly different failure mechanisms in the vicinity of the fibre matrix interface for the bio-epoxy (interfacial) and the thermoplastic (cohesive). Overall, both matrices show promise in terms of fatigue performance under benign laboratory conditions and as a stepping stone towards achieving more sustainable matrix options for offshore renewable energy structures in the future.</div></div>","PeriodicalId":34525,"journal":{"name":"Composites Part C Open Access","volume":"17 ","pages":"Article 100608"},"PeriodicalIF":5.3,"publicationDate":"2025-07-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"144108003","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
Delamination is among the most prevalent life-limiting failure modes in laminated composites. Mode II delaminations, driven by in-plane shear loads, are more difficult to observe than mode I delaminations. Conventional edge observation techniques fail to capture the three-dimensional (3D) delamination front and its associated damage mechanisms. We conduct the first in situ X-ray computed tomography (CT) experiment to observe the 3D development of delamination under mode II loading. We apply four-point end-notched flexure loading to two types of thin-ply, carbon-fibre-reinforced composite laminates: a 0° laminate and a cross-ply laminate susceptible to delamination migration. The method is proven capable of capturing delamination growth and migration within the bulk of the laminates at the meso- and microscale, something unattainable using conventional techniques. This work thus demonstrates the benefits of in situ CT in determining the damage mechanisms involved in mode II fracture loading.
{"title":"3D observation of delamination in carbon-fibre-reinforced composites under mode II loading through in situ computed tomography","authors":"Panayiotis Tsokanas, Thanasis Chatziathanasiou, Yentl Swolfs","doi":"10.1016/j.jcomc.2025.100615","DOIUrl":"10.1016/j.jcomc.2025.100615","url":null,"abstract":"<div><div>Delamination is among the most prevalent life-limiting failure modes in laminated composites. Mode II delaminations, driven by in-plane shear loads, are more difficult to observe than mode I delaminations. Conventional edge observation techniques fail to capture the three-dimensional (3D) delamination front and its associated damage mechanisms. We conduct the first in situ X-ray computed tomography (CT) experiment to observe the 3D development of delamination under mode II loading. We apply four-point end-notched flexure loading to two types of thin-ply, carbon-fibre-reinforced composite laminates: a 0° laminate and a cross-ply laminate susceptible to delamination migration. The method is proven capable of capturing delamination growth and migration within the bulk of the laminates at the meso- and microscale, something unattainable using conventional techniques. This work thus demonstrates the benefits of in situ CT in determining the damage mechanisms involved in mode II fracture loading.</div></div>","PeriodicalId":34525,"journal":{"name":"Composites Part C Open Access","volume":"17 ","pages":"Article 100615"},"PeriodicalIF":5.3,"publicationDate":"2025-07-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"144313006","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
Pub Date : 2025-07-01Epub Date: 2025-06-03DOI: 10.1016/j.jcomc.2025.100616
Nour Ghazal Aswad , Mohammed Al Dawood , Farid Abed
Fiber-reinforced polymer (FRP) reinforcement has gained significant attention in research and structural applications due to its desirable mechanical properties and durability. Advances have been made in understanding FRP’s resistance to elevated temperatures; however, uncertainties persist due to inconsistencies in the available experimental data. This study presents an experimental investigation into the effects of various parameters on the performance of reinforced concrete (RC) prismatic beams exposed to elevated temperatures. Key parameters included reinforcement type (steel, Glass FRP (GFRP), and Basalt FRP (BFRP), bar diameter (16 mm and 20 mm), surface texture (ribbed and sand-coated), and concrete cover (40 mm and 60 mm). The prismatic beams were subjected to target temperatures of 200, 400, and 700 °C, followed by testing in a four-point loading setup. The experimental results revealed that BFRP-reinforced prismatic beams exhibited a 17 % higher residual load-carrying capacity and 32.3 % greater toughness at 200 °C and 400 °C, but a 22 % lower capacity and 26.9 % reduction in toughness at 700 °C compared to their GFRP-reinforced counterparts. Additionally, prismatic beams reinforced with sand-coated GFRP bars showed up to a 27 % improvement in load-carrying capacity compared to those with ribbed GFRP bars, and a larger concrete cover contributed to better overall flexural performance of the prismatic beams under elevated temperatures.
{"title":"Effects of elevated temperature on basalt and glass FRP bars in prismatic beams under flexural loading","authors":"Nour Ghazal Aswad , Mohammed Al Dawood , Farid Abed","doi":"10.1016/j.jcomc.2025.100616","DOIUrl":"10.1016/j.jcomc.2025.100616","url":null,"abstract":"<div><div>Fiber-reinforced polymer (FRP) reinforcement has gained significant attention in research and structural applications due to its desirable mechanical properties and durability. Advances have been made in understanding FRP’s resistance to elevated temperatures; however, uncertainties persist due to inconsistencies in the available experimental data. This study presents an experimental investigation into the effects of various parameters on the performance of reinforced concrete (RC) prismatic beams exposed to elevated temperatures. Key parameters included reinforcement type (steel, Glass FRP (GFRP), and Basalt FRP (BFRP), bar diameter (16 mm and 20 mm), surface texture (ribbed and sand-coated), and concrete cover (40 mm and 60 mm). The prismatic beams were subjected to target temperatures of 200, 400, and 700 °C, followed by testing in a four-point loading setup. The experimental results revealed that BFRP-reinforced prismatic beams exhibited a 17 % higher residual load-carrying capacity and 32.3 % greater toughness at 200 °C and 400 °C, but a 22 % lower capacity and 26.9 % reduction in toughness at 700 °C compared to their GFRP-reinforced counterparts. Additionally, prismatic beams reinforced with sand-coated GFRP bars showed up to a 27 % improvement in load-carrying capacity compared to those with ribbed GFRP bars, and a larger concrete cover contributed to better overall flexural performance of the prismatic beams under elevated temperatures.</div></div>","PeriodicalId":34525,"journal":{"name":"Composites Part C Open Access","volume":"17 ","pages":"Article 100616"},"PeriodicalIF":5.3,"publicationDate":"2025-07-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"144221026","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
Pub Date : 2025-07-01Epub Date: 2025-06-19DOI: 10.1016/j.jcomc.2025.100623
Mehrnoosh Javadian, Ali Dadashi, Abbasali Bagheri, Mohammad Azadi
This study investigates the fatigue behavior and failure mechanisms of 3D-printed polylactic acid (PLA) composites reinforced with continuous glass fibers under rotating bending fatigue. Composite specimens were fabricated using a modified fused deposition modeling (FDM) printer with fiber volume fractions of 16 %. Fatigue testing was conducted under fully reversed loading at room temperature, and fracture surfaces were analyzed using field-emission scanning electron microscopy (FE-SEM). Results indicate that fiber reinforcement significantly enhances fatigue resistance, with fiber orientation (+45/-45) and infill density playing critical roles in improving performance. A Poisson regression model confirmed the statistical significance of all main effects and two interactions, with print direction having the greatest influence. Fractographic analysis revealed void, fiber breakage, and fiber-matrix debonding as key failure modes. The study provides crucial insights for optimizing composite materials for applications involving cyclic loading.
{"title":"Fatigue behavior and failure mechanism of 3D-printed continuous glass fiber-reinforced PLA composites under rotating bending fatigue","authors":"Mehrnoosh Javadian, Ali Dadashi, Abbasali Bagheri, Mohammad Azadi","doi":"10.1016/j.jcomc.2025.100623","DOIUrl":"10.1016/j.jcomc.2025.100623","url":null,"abstract":"<div><div>This study investigates the fatigue behavior and failure mechanisms of 3D-printed polylactic acid (PLA) composites reinforced with continuous glass fibers under rotating bending fatigue. Composite specimens were fabricated using a modified fused deposition modeling (FDM) printer with fiber volume fractions of 16 %. Fatigue testing was conducted under fully reversed loading at room temperature, and fracture surfaces were analyzed using field-emission scanning electron microscopy (FE-SEM). Results indicate that fiber reinforcement significantly enhances fatigue resistance, with fiber orientation (+45/-45) and infill density playing critical roles in improving performance. A Poisson regression model confirmed the statistical significance of all main effects and two interactions, with print direction having the greatest influence. Fractographic analysis revealed void, fiber breakage, and fiber-matrix debonding as key failure modes. The study provides crucial insights for optimizing composite materials for applications involving cyclic loading.</div></div>","PeriodicalId":34525,"journal":{"name":"Composites Part C Open Access","volume":"17 ","pages":"Article 100623"},"PeriodicalIF":5.3,"publicationDate":"2025-07-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"144523030","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
A pin-ended buckling test inspired by Wisnom [1] was developed to evaluate the effect of strain gradient on the compressive failure strain of composite laminates. Tests were conducted on unidirectional (UD) carbon/epoxy AS4/8552, and strain measurements were obtained using digital image correlation. Various cross-ply stacking sequences, [(0/90)₂]S, [(0/90)₄]S, [(0/90)₈]S, were studied and most specimens failed on the tension side due to the high compressive strength facilitated by the strain gradient, while the tensile failure strain remained unaffected by the strain gradient. To induce failure on the compression side, a novel method was developed by manufacturing bi-material specimens with an aluminum 2024 ply added to the tension side. This modification led to all bi-material specimens failing on the compression side. The results showed a Nnar increase in compressive failure strain as a function of the strain gradient. Furthermore, values reaching up to -33,000 microstrains were obtained for the thinner specimens, which is >2.5 times the compressive failure strain of -12,500 microstrains announced by the manufacturer. This behavior is new compared to other published results obtained on similarly tested materials that demonstrated a linear trend.
{"title":"Evaluation of the strain gradient effect on compressive failure of CRFP composites","authors":"Tobias Bianchi , Jawad Naciri , Joël Serra , Christophe Bouvet , Léon Ratsifandriahana","doi":"10.1016/j.jcomc.2025.100621","DOIUrl":"10.1016/j.jcomc.2025.100621","url":null,"abstract":"<div><div>A pin-ended buckling test inspired by Wisnom [<span><span>1</span></span>] was developed to evaluate the effect of strain gradient on the compressive failure strain of composite laminates. Tests were conducted on unidirectional (UD) carbon/epoxy AS4/8552, and strain measurements were obtained using digital image correlation. Various cross-ply stacking sequences, [(0/90)₂]<sub>S</sub>, [(0/90)₄]<sub>S</sub>, [(0/90)₈]<sub>S</sub>, were studied and most specimens failed on the tension side due to the high compressive strength facilitated by the strain gradient, while the tensile failure strain remained unaffected by the strain gradient. To induce failure on the compression side, a novel method was developed by manufacturing bi-material specimens with an aluminum 2024 ply added to the tension side. This modification led to all bi-material specimens failing on the compression side. The results showed a Nnar increase in compressive failure strain as a function of the strain gradient. Furthermore, values reaching up to -33,000 microstrains were obtained for the thinner specimens, which is >2.5 times the compressive failure strain of -12,500 microstrains announced by the manufacturer. This behavior is new compared to other published results obtained on similarly tested materials that demonstrated a linear trend.</div></div>","PeriodicalId":34525,"journal":{"name":"Composites Part C Open Access","volume":"17 ","pages":"Article 100621"},"PeriodicalIF":5.3,"publicationDate":"2025-07-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"144470594","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
Pub Date : 2025-07-01Epub Date: 2025-07-26DOI: 10.1016/j.jcomc.2025.100631
Koranat Pattarakunnan , Joel L. Galos , Raj Das
Multifunctional carbon fibre reinforced polymer (CFRP) composite structures with embedded batteries can simultaneously carry mechanical loads and store and supply electrical energy have future potential applications in electric vehicles. This paper conducts a parametric study of CFRP laminates with embedded batteries using a finite element (FE) model that has been experimentally validated. The parametric study investigated the effects of number of embedded lithium-ion (Li-ion) polymer (LiPo) batteries (up to 400 batteries), their locations (up to a grid of 20 × 20 batteries) and thicknesses (4 mm, 2 mm and 1 mm), as well as CFRP fibre stacking sequences ([0],[0/90],[0/±45/90] and [±45]) on specific stiffness and strength (density normalised) and gravimetric energy density of multifunctional CFRP laminates. A similar FE parametric study on a curved CFRP vehicle roof with embedded batteries was also conducted. Embedded batteries can provide energy density of up to about 75 Wh/kg and 20 Wh/kg when 20 × 20 batteries were embedded in CFRP laminates and CFRP roof, respectively. However, they had adverse effects on specific mechanical properties of both CFRP laminates and CFRP roof with embedded batteries. It was suggested that the thickness of the embedded batteries should be carefully picked to achieve an optimal trade-off between desired energy density and resultant specific mechanical properties.
{"title":"Design and analysis of energy storage multifunctional composite structures with embedded lithium-ion batteries","authors":"Koranat Pattarakunnan , Joel L. Galos , Raj Das","doi":"10.1016/j.jcomc.2025.100631","DOIUrl":"10.1016/j.jcomc.2025.100631","url":null,"abstract":"<div><div>Multifunctional carbon fibre reinforced polymer (CFRP) composite structures with embedded batteries can simultaneously carry mechanical loads and store and supply electrical energy have future potential applications in electric vehicles. This paper conducts a parametric study of CFRP laminates with embedded batteries using a finite element (FE) model that has been experimentally validated. The parametric study investigated the effects of number of embedded lithium-ion (Li-ion) polymer (LiPo) batteries (up to 400 batteries), their locations (up to a grid of 20 × 20 batteries) and thicknesses (4 mm, 2 mm and 1 mm), as well as CFRP fibre stacking sequences ([0],[0/90],[0/±45/90] and [±45]) on specific stiffness and strength (density normalised) and gravimetric energy density of multifunctional CFRP laminates. A similar FE parametric study on a curved CFRP vehicle roof with embedded batteries was also conducted. Embedded batteries can provide energy density of up to about 75 Wh/kg and 20 Wh/kg when 20 × 20 batteries were embedded in CFRP laminates and CFRP roof, respectively. However, they had adverse effects on specific mechanical properties of both CFRP laminates and CFRP roof with embedded batteries. It was suggested that the thickness of the embedded batteries should be carefully picked to achieve an optimal trade-off between desired energy density and resultant specific mechanical properties.</div></div>","PeriodicalId":34525,"journal":{"name":"Composites Part C Open Access","volume":"17 ","pages":"Article 100631"},"PeriodicalIF":7.0,"publicationDate":"2025-07-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"144723075","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
Pub Date : 2025-07-01Epub Date: 2025-04-11DOI: 10.1016/j.jcomc.2025.100595
Nanci Ehman , Sandra Rodríguez Fabià , Julia Catalán , Gary Chinga-Carrasco
Wood-derived components (e.g. fibers, lignin, nanofibers) are widely studied to develop thermoplastic biocomposites with, for example, improved mechanical properties and reduced global warming potential. Manufacturing of biocomposite products includes compounding and conversion processes (e.g., extrusion, injection molding, and 3D printing). These processes apply mechanical forces and heat to melt thermoplastic polymers and form a given product. However, in some cases, compounding and conversion stages may generate emissions of volatile organic compounds (VOC) and/or ultrafine particles (UFP) and we must consider their effects on human health. Additionally, due to the nano-dimensions cellulose nanofibers are considered UFP. Therefore, its impacts on human health should be evaluated, especially when dried for biocomposite production. This review provides an overview of emissions generated in the production line of lignocellulose-based biocomposites, considering: wood preprocessing, extrusion, 3D printing, and injection moulding. Emissions of VOCs and UFP were considered, including the occupational exposure limits according to the current regulations and the potential health effects associated with such emissions
{"title":"Emission risks in processing and conversion of lignocellulose-based biocomposites","authors":"Nanci Ehman , Sandra Rodríguez Fabià , Julia Catalán , Gary Chinga-Carrasco","doi":"10.1016/j.jcomc.2025.100595","DOIUrl":"10.1016/j.jcomc.2025.100595","url":null,"abstract":"<div><div>Wood-derived components (e.g. fibers, lignin, nanofibers) are widely studied to develop thermoplastic biocomposites with, for example, improved mechanical properties and reduced global warming potential. Manufacturing of biocomposite products includes compounding and conversion processes (e.g., extrusion, injection molding, and 3D printing). These processes apply mechanical forces and heat to melt thermoplastic polymers and form a given product. However, in some cases, compounding and conversion stages may generate emissions of volatile organic compounds (VOC) and/or ultrafine particles (UFP) and we must consider their effects on human health. Additionally, due to the nano-dimensions cellulose nanofibers are considered UFP. Therefore, its impacts on human health should be evaluated, especially when dried for biocomposite production. This review provides an overview of emissions generated in the production line of lignocellulose-based biocomposites, considering: wood preprocessing, extrusion, 3D printing, and injection moulding. Emissions of VOCs and UFP were considered, including the occupational exposure limits according to the current regulations and the potential health effects associated with such emissions</div></div>","PeriodicalId":34525,"journal":{"name":"Composites Part C Open Access","volume":"17 ","pages":"Article 100595"},"PeriodicalIF":5.3,"publicationDate":"2025-07-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"143843270","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
Pub Date : 2025-07-01Epub Date: 2025-06-18DOI: 10.1016/j.jcomc.2025.100620
Boxin Chang , Shuaixing Wang , Gaoge Liang , Quanxing Liu , Yong Xiao
Low-frequency sound insulation is one of the most challenging problems in the field of noise control engineering because of the classical mass law. Recent studies have shown that acoustic metamaterials can achieve a sound transmission loss (STL) higher than the mass law at specific low frequencies. However, it is still difficult to realize superior STL that can deeply break the mass law over a broadband low-frequency range, especially under the excitation of diffuse field sound. To challenge this problem, we suggest a multilayer composite plate-type metamaterial (MCPM) consisting of two single-layer metamaterial plates and a sandwiched layer of porous material. The metamaterial plates are simply constructed by a thin plate attached with periodic strip masses. We present an in-depth theoretical analysis and experimental verification of the STL performance of the MCPM. The results indicate that with proper design, the MCPM can achieve an excellent diffuse STL over an ultra-broadband low-frequency range, while avoiding the significant reduction of immediately following high-frequency STL. Owing to its simple construction yet superior low-frequency diffuse sound insulation performance, the MCPM can find promising applications in noise control engineering.
{"title":"Broadband low-frequency diffuse sound transmission loss of multilayer composite plate-type metamaterials","authors":"Boxin Chang , Shuaixing Wang , Gaoge Liang , Quanxing Liu , Yong Xiao","doi":"10.1016/j.jcomc.2025.100620","DOIUrl":"10.1016/j.jcomc.2025.100620","url":null,"abstract":"<div><div>Low-frequency sound insulation is one of the most challenging problems in the field of noise control engineering because of the classical mass law. Recent studies have shown that acoustic metamaterials can achieve a sound transmission loss (STL) higher than the mass law at specific low frequencies. However, it is still difficult to realize superior STL that can deeply break the mass law over a broadband low-frequency range, especially under the excitation of diffuse field sound. To challenge this problem, we suggest a multilayer composite plate-type metamaterial (MCPM) consisting of two single-layer metamaterial plates and a sandwiched layer of porous material. The metamaterial plates are simply constructed by a thin plate attached with periodic strip masses. We present an in-depth theoretical analysis and experimental verification of the STL performance of the MCPM. The results indicate that with proper design, the MCPM can achieve an excellent diffuse STL over an ultra-broadband low-frequency range, while avoiding the significant reduction of immediately following high-frequency STL. Owing to its simple construction yet superior low-frequency diffuse sound insulation performance, the MCPM can find promising applications in noise control engineering.</div></div>","PeriodicalId":34525,"journal":{"name":"Composites Part C Open Access","volume":"17 ","pages":"Article 100620"},"PeriodicalIF":5.3,"publicationDate":"2025-07-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"144331202","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
Pub Date : 2025-07-01Epub Date: 2025-07-16DOI: 10.1016/j.jcomc.2025.100627
Balázs Markó , Szilárd Seprős , Jinyang Xu , Norbert Geier
Aluminium/carbon fibre reinforced polymer (Al/CFRP) composite stacks combine the high strength-to-weight ratio of the CFRP with the ductility and impact resistance of aluminium. Due to their excellent mechanical properties, Al/CFRP stacks are becoming increasingly popular in major industrial fields such as aerospace and automotive. However, mechanical machining of these materials, particularly at the interlayer regions, presents significant challenges, notably the formation of interlayer burrs. To address this issue, we introduce an innovative hole-making technology designed to minimise machining-induced interlayer burr formation. The novel technology integrates helical and spiral interpolation strategies to reduce axial force at the interlayer interfaces. We validated the efficiency of the novel technology through a series of machining experiments, employing a Central Composite Inscribed (CCI) experimental design. The experiments were performed on a three-axis CNC milling centre, with burr measurements obtained using a Keyence VR-5000 3D profilometer. Maximum burr heights were recorded along the hole contours at one-degree intervals. Our findings demonstrate a significant reduction (28 %) in interlayer burr formation in unidirectional carbon fibre-reinforced polymer (UD-CFRP) plates when utilising the proposed technique. These results suggest that our developed method is promising to improve machining quality in Al/CFRP stacks, meriting further investigation and development.
{"title":"Effective suppression of machining-induced interlayer damage in machined holes of Al/CFRP stacks","authors":"Balázs Markó , Szilárd Seprős , Jinyang Xu , Norbert Geier","doi":"10.1016/j.jcomc.2025.100627","DOIUrl":"10.1016/j.jcomc.2025.100627","url":null,"abstract":"<div><div>Aluminium/carbon fibre reinforced polymer (Al/CFRP) composite stacks combine the high strength-to-weight ratio of the CFRP with the ductility and impact resistance of aluminium. Due to their excellent mechanical properties, Al/CFRP stacks are becoming increasingly popular in major industrial fields such as aerospace and automotive. However, mechanical machining of these materials, particularly at the interlayer regions, presents significant challenges, notably the formation of interlayer burrs. To address this issue, we introduce an innovative hole-making technology designed to minimise machining-induced interlayer burr formation. The novel technology integrates helical and spiral interpolation strategies to reduce axial force at the interlayer interfaces. We validated the efficiency of the novel technology through a series of machining experiments, employing a Central Composite Inscribed (CCI) experimental design. The experiments were performed on a three-axis CNC milling centre, with burr measurements obtained using a Keyence VR-5000 3D profilometer. Maximum burr heights were recorded along the hole contours at one-degree intervals. Our findings demonstrate a significant reduction (28 %) in interlayer burr formation in unidirectional carbon fibre-reinforced polymer (UD-CFRP) plates when utilising the proposed technique. These results suggest that our developed method is promising to improve machining quality in Al/CFRP stacks, meriting further investigation and development.</div></div>","PeriodicalId":34525,"journal":{"name":"Composites Part C Open Access","volume":"17 ","pages":"Article 100627"},"PeriodicalIF":5.3,"publicationDate":"2025-07-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"144665919","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
Pub Date : 2025-07-01Epub Date: 2025-04-28DOI: 10.1016/j.jcomc.2025.100596
Kishor B. Shingare , Suhas Alkunte , Baosong Li , Andreas Schiffer , Ian Kinloch , Kin Liao
Owing to their superior electro-thermo-mechanical properties, the significance of interpenetrating phase composites (IPCs) in various industries is in high demand. IPCs, characterized by infiltrating metal, ceramic, and polymer phases, provide various advantages, including a balanced mixture of strength, stiffness, and toughness, excellent thermal characteristics, wear resistance, and flexibility in microstructure and processing routes. This comprehensive review explores the realm of multifunctional reinforcing phases, specifically focusing on their integration into 3D printed composites. Within this context, the IPCs with a special spotlight on captivating world of Triply Periodic Minimal Surface (TPMS) and other cellular/lattice architectures wherein two core themes are presented and dissected: TPMS-based IPCs, which collaboratively amplify properties of another phase and interpenetrating piezoelectric phase composites (IP2Cs), which offer special advantages over conventional ones. We compiled comprehensive data on IPCs, emphasizing their effective properties, mechanical performance, fatigue and fracture behavior, energy absorption capacity, and coupled electromechanical characteristics. Furthermore, the commercial applications of architectured IPCs across industries are highlighted, along with a critical analysis of current research, identifying gaps and challenges. It highlights their pivotal role in advancing technology and addressing contemporary challenges while illuminating the uncharted possibilities presented by TPMS cellular structures in the dynamic landscape of 3D printing.
{"title":"Multifunctional TPMS-based interpenetrating phase composites: A comprehensive review of structure, properties, piezoelectricity and applications","authors":"Kishor B. Shingare , Suhas Alkunte , Baosong Li , Andreas Schiffer , Ian Kinloch , Kin Liao","doi":"10.1016/j.jcomc.2025.100596","DOIUrl":"10.1016/j.jcomc.2025.100596","url":null,"abstract":"<div><div>Owing to their superior electro-thermo-mechanical properties, the significance of interpenetrating phase composites (IPCs) in various industries is in high demand. IPCs, characterized by infiltrating metal, ceramic, and polymer phases, provide various advantages, including a balanced mixture of strength, stiffness, and toughness, excellent thermal characteristics, wear resistance, and flexibility in microstructure and processing routes. This comprehensive review explores the realm of multifunctional reinforcing phases, specifically focusing on their integration into 3D printed composites. Within this context, the IPCs with a special spotlight on captivating world of Triply Periodic Minimal Surface (TPMS) and other cellular/lattice architectures wherein two core themes are presented and dissected: TPMS-based IPCs, which collaboratively amplify properties of another phase and interpenetrating piezoelectric phase composites (IP<sup>2</sup>Cs), which offer special advantages over conventional ones. We compiled comprehensive data on IPCs, emphasizing their effective properties, mechanical performance, fatigue and fracture behavior, energy absorption capacity, and coupled electromechanical characteristics. Furthermore, the commercial applications of architectured IPCs across industries are highlighted, along with a critical analysis of current research, identifying gaps and challenges. It highlights their pivotal role in advancing technology and addressing contemporary challenges while illuminating the uncharted possibilities presented by TPMS cellular structures in the dynamic landscape of 3D printing.</div></div>","PeriodicalId":34525,"journal":{"name":"Composites Part C Open Access","volume":"17 ","pages":"Article 100596"},"PeriodicalIF":5.3,"publicationDate":"2025-07-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"143882447","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}