Effect of the Matrix on the Properties of Carbon Fiber Reinforced Plastics
Abstract The effect of rigid and flexible matrices on the properties of carbon fiber reinforced plastics has been studied using the impact break method at different rates of loading the composite material (CM). It has been established that the strain of CM under static loading conditions has a smoot...
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| Autor*in: |
Korneeva, N. V. [verfasserIn] |
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| Format: |
E-Artikel |
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| Sprache: |
Englisch |
| Erschienen: |
2019 |
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| Anmerkung: |
© Pleiades Publishing, Ltd. 2019 |
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| Übergeordnetes Werk: |
Enthalten in: Russian journal of physical chemistry - Moscow : MAIK Nauka, Interperiodica Publ., 2007, 13(2019), 5 vom: Sept., Seite 838-841 |
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| Übergeordnetes Werk: |
volume:13 ; year:2019 ; number:5 ; month:09 ; pages:838-841 |
| Links: |
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| DOI / URN: |
10.1134/S1990793119050038 |
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SPR022589910 |
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| 520 | |a Abstract The effect of rigid and flexible matrices on the properties of carbon fiber reinforced plastics has been studied using the impact break method at different rates of loading the composite material (CM). It has been established that the strain of CM under static loading conditions has a smooth character and is generally tensile. For this reason, CM with a plastic matrix under static loading conditions has higher properties, such as the maximum specific absorbed-in-fracture energy α = 154 J/$ cm^{2} $ and the maximum strength σ = 524 MPa at a greater relative strain ε = 6%. The fracture mechanism of carbon fiber reinforced plastics (CFRPs) abruptly changes upon an impact. The fracture of CMs is initiated by an impact at the first moment of its action. The entire process of CM strain until fracture is accompanied by fiber filament breaks. Load fluctuations occur due to filament breaks and are reflected in the strain curves in the form of peaks. The processes of filament break and crush are superimposed on the overall process of multistage CM tensile strain at a higher level. The accumulation of fiber crushes and breaks decreases the strength of CMs. This leads to fast fracture at lower strain in comparison with the case of static loading conditions. The specific absorbed-in-fracture energy α of CFRPs with a flexible matrix decreases upon an impact by a factor of 3.4, from 154 to 45 J/$ cm^{2} $, relative to the specific absorbed-in-fracture energy of CM in the static case; the material is fractured at a smaller relative strain ε = 1.7% and a lower strength σ = 496 MPa. | ||
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| 700 | 1 | |a Krylov, I. K. |4 aut | |
| 700 | 1 | |a Mamonov, V. I. |4 aut | |
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10.1134/S1990793119050038 doi (DE-627)SPR022589910 (SPR)S1990793119050038-e DE-627 ger DE-627 rakwb eng Korneeva, N. V. verfasserin aut Effect of the Matrix on the Properties of Carbon Fiber Reinforced Plastics 2019 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier © Pleiades Publishing, Ltd. 2019 Abstract The effect of rigid and flexible matrices on the properties of carbon fiber reinforced plastics has been studied using the impact break method at different rates of loading the composite material (CM). It has been established that the strain of CM under static loading conditions has a smooth character and is generally tensile. For this reason, CM with a plastic matrix under static loading conditions has higher properties, such as the maximum specific absorbed-in-fracture energy α = 154 J/$ cm^{2} $ and the maximum strength σ = 524 MPa at a greater relative strain ε = 6%. The fracture mechanism of carbon fiber reinforced plastics (CFRPs) abruptly changes upon an impact. The fracture of CMs is initiated by an impact at the first moment of its action. The entire process of CM strain until fracture is accompanied by fiber filament breaks. Load fluctuations occur due to filament breaks and are reflected in the strain curves in the form of peaks. The processes of filament break and crush are superimposed on the overall process of multistage CM tensile strain at a higher level. The accumulation of fiber crushes and breaks decreases the strength of CMs. This leads to fast fracture at lower strain in comparison with the case of static loading conditions. The specific absorbed-in-fracture energy α of CFRPs with a flexible matrix decreases upon an impact by a factor of 3.4, from 154 to 45 J/$ cm^{2} $, relative to the specific absorbed-in-fracture energy of CM in the static case; the material is fractured at a smaller relative strain ε = 1.7% and a lower strength σ = 496 MPa. Kudinov, V. V. aut Krylov, I. K. aut Mamonov, V. I. aut Enthalten in Russian journal of physical chemistry Moscow : MAIK Nauka, Interperiodica Publ., 2007 13(2019), 5 vom: Sept., Seite 838-841 (DE-627)688079938 (DE-600)2653166-5 1990-7923 nnns volume:13 year:2019 number:5 month:09 pages:838-841 https://dx.doi.org/10.1134/S1990793119050038 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_SPRINGER SSG-OLC-PHA GBV_ILN_11 GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_32 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_74 GBV_ILN_90 GBV_ILN_95 GBV_ILN_100 GBV_ILN_101 GBV_ILN_105 GBV_ILN_110 GBV_ILN_120 GBV_ILN_138 GBV_ILN_150 GBV_ILN_151 GBV_ILN_152 GBV_ILN_161 GBV_ILN_170 GBV_ILN_171 GBV_ILN_187 GBV_ILN_213 GBV_ILN_224 GBV_ILN_230 GBV_ILN_250 GBV_ILN_281 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_636 GBV_ILN_702 GBV_ILN_2001 GBV_ILN_2003 GBV_ILN_2004 GBV_ILN_2005 GBV_ILN_2006 GBV_ILN_2007 GBV_ILN_2008 GBV_ILN_2009 GBV_ILN_2010 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_2025 GBV_ILN_2026 GBV_ILN_2027 GBV_ILN_2031 GBV_ILN_2034 GBV_ILN_2037 GBV_ILN_2038 GBV_ILN_2039 GBV_ILN_2044 GBV_ILN_2048 GBV_ILN_2049 GBV_ILN_2050 GBV_ILN_2055 GBV_ILN_2057 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 GBV_ILN_2070 GBV_ILN_2086 GBV_ILN_2088 GBV_ILN_2093 GBV_ILN_2106 GBV_ILN_2107 GBV_ILN_2108 GBV_ILN_2110 GBV_ILN_2111 GBV_ILN_2112 GBV_ILN_2113 GBV_ILN_2116 GBV_ILN_2118 GBV_ILN_2119 GBV_ILN_2122 GBV_ILN_2129 GBV_ILN_2143 GBV_ILN_2144 GBV_ILN_2147 GBV_ILN_2148 GBV_ILN_2152 GBV_ILN_2153 GBV_ILN_2188 GBV_ILN_2190 GBV_ILN_2232 GBV_ILN_2336 GBV_ILN_2446 GBV_ILN_2470 GBV_ILN_2472 GBV_ILN_2507 GBV_ILN_2522 GBV_ILN_2548 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4046 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4242 GBV_ILN_4246 GBV_ILN_4249 GBV_ILN_4251 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4326 GBV_ILN_4333 GBV_ILN_4334 GBV_ILN_4335 GBV_ILN_4336 GBV_ILN_4338 GBV_ILN_4393 GBV_ILN_4700 AR 13 2019 5 09 838-841 |
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10.1134/S1990793119050038 doi (DE-627)SPR022589910 (SPR)S1990793119050038-e DE-627 ger DE-627 rakwb eng Korneeva, N. V. verfasserin aut Effect of the Matrix on the Properties of Carbon Fiber Reinforced Plastics 2019 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier © Pleiades Publishing, Ltd. 2019 Abstract The effect of rigid and flexible matrices on the properties of carbon fiber reinforced plastics has been studied using the impact break method at different rates of loading the composite material (CM). It has been established that the strain of CM under static loading conditions has a smooth character and is generally tensile. For this reason, CM with a plastic matrix under static loading conditions has higher properties, such as the maximum specific absorbed-in-fracture energy α = 154 J/$ cm^{2} $ and the maximum strength σ = 524 MPa at a greater relative strain ε = 6%. The fracture mechanism of carbon fiber reinforced plastics (CFRPs) abruptly changes upon an impact. The fracture of CMs is initiated by an impact at the first moment of its action. The entire process of CM strain until fracture is accompanied by fiber filament breaks. Load fluctuations occur due to filament breaks and are reflected in the strain curves in the form of peaks. The processes of filament break and crush are superimposed on the overall process of multistage CM tensile strain at a higher level. The accumulation of fiber crushes and breaks decreases the strength of CMs. This leads to fast fracture at lower strain in comparison with the case of static loading conditions. The specific absorbed-in-fracture energy α of CFRPs with a flexible matrix decreases upon an impact by a factor of 3.4, from 154 to 45 J/$ cm^{2} $, relative to the specific absorbed-in-fracture energy of CM in the static case; the material is fractured at a smaller relative strain ε = 1.7% and a lower strength σ = 496 MPa. Kudinov, V. V. aut Krylov, I. K. aut Mamonov, V. I. aut Enthalten in Russian journal of physical chemistry Moscow : MAIK Nauka, Interperiodica Publ., 2007 13(2019), 5 vom: Sept., Seite 838-841 (DE-627)688079938 (DE-600)2653166-5 1990-7923 nnns volume:13 year:2019 number:5 month:09 pages:838-841 https://dx.doi.org/10.1134/S1990793119050038 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_SPRINGER SSG-OLC-PHA GBV_ILN_11 GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_32 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_74 GBV_ILN_90 GBV_ILN_95 GBV_ILN_100 GBV_ILN_101 GBV_ILN_105 GBV_ILN_110 GBV_ILN_120 GBV_ILN_138 GBV_ILN_150 GBV_ILN_151 GBV_ILN_152 GBV_ILN_161 GBV_ILN_170 GBV_ILN_171 GBV_ILN_187 GBV_ILN_213 GBV_ILN_224 GBV_ILN_230 GBV_ILN_250 GBV_ILN_281 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_636 GBV_ILN_702 GBV_ILN_2001 GBV_ILN_2003 GBV_ILN_2004 GBV_ILN_2005 GBV_ILN_2006 GBV_ILN_2007 GBV_ILN_2008 GBV_ILN_2009 GBV_ILN_2010 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_2025 GBV_ILN_2026 GBV_ILN_2027 GBV_ILN_2031 GBV_ILN_2034 GBV_ILN_2037 GBV_ILN_2038 GBV_ILN_2039 GBV_ILN_2044 GBV_ILN_2048 GBV_ILN_2049 GBV_ILN_2050 GBV_ILN_2055 GBV_ILN_2057 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 GBV_ILN_2070 GBV_ILN_2086 GBV_ILN_2088 GBV_ILN_2093 GBV_ILN_2106 GBV_ILN_2107 GBV_ILN_2108 GBV_ILN_2110 GBV_ILN_2111 GBV_ILN_2112 GBV_ILN_2113 GBV_ILN_2116 GBV_ILN_2118 GBV_ILN_2119 GBV_ILN_2122 GBV_ILN_2129 GBV_ILN_2143 GBV_ILN_2144 GBV_ILN_2147 GBV_ILN_2148 GBV_ILN_2152 GBV_ILN_2153 GBV_ILN_2188 GBV_ILN_2190 GBV_ILN_2232 GBV_ILN_2336 GBV_ILN_2446 GBV_ILN_2470 GBV_ILN_2472 GBV_ILN_2507 GBV_ILN_2522 GBV_ILN_2548 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4046 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4242 GBV_ILN_4246 GBV_ILN_4249 GBV_ILN_4251 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4326 GBV_ILN_4333 GBV_ILN_4334 GBV_ILN_4335 GBV_ILN_4336 GBV_ILN_4338 GBV_ILN_4393 GBV_ILN_4700 AR 13 2019 5 09 838-841 |
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10.1134/S1990793119050038 doi (DE-627)SPR022589910 (SPR)S1990793119050038-e DE-627 ger DE-627 rakwb eng Korneeva, N. V. verfasserin aut Effect of the Matrix on the Properties of Carbon Fiber Reinforced Plastics 2019 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier © Pleiades Publishing, Ltd. 2019 Abstract The effect of rigid and flexible matrices on the properties of carbon fiber reinforced plastics has been studied using the impact break method at different rates of loading the composite material (CM). It has been established that the strain of CM under static loading conditions has a smooth character and is generally tensile. For this reason, CM with a plastic matrix under static loading conditions has higher properties, such as the maximum specific absorbed-in-fracture energy α = 154 J/$ cm^{2} $ and the maximum strength σ = 524 MPa at a greater relative strain ε = 6%. The fracture mechanism of carbon fiber reinforced plastics (CFRPs) abruptly changes upon an impact. The fracture of CMs is initiated by an impact at the first moment of its action. The entire process of CM strain until fracture is accompanied by fiber filament breaks. Load fluctuations occur due to filament breaks and are reflected in the strain curves in the form of peaks. The processes of filament break and crush are superimposed on the overall process of multistage CM tensile strain at a higher level. The accumulation of fiber crushes and breaks decreases the strength of CMs. This leads to fast fracture at lower strain in comparison with the case of static loading conditions. The specific absorbed-in-fracture energy α of CFRPs with a flexible matrix decreases upon an impact by a factor of 3.4, from 154 to 45 J/$ cm^{2} $, relative to the specific absorbed-in-fracture energy of CM in the static case; the material is fractured at a smaller relative strain ε = 1.7% and a lower strength σ = 496 MPa. Kudinov, V. V. aut Krylov, I. K. aut Mamonov, V. I. aut Enthalten in Russian journal of physical chemistry Moscow : MAIK Nauka, Interperiodica Publ., 2007 13(2019), 5 vom: Sept., Seite 838-841 (DE-627)688079938 (DE-600)2653166-5 1990-7923 nnns volume:13 year:2019 number:5 month:09 pages:838-841 https://dx.doi.org/10.1134/S1990793119050038 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_SPRINGER SSG-OLC-PHA GBV_ILN_11 GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_32 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_74 GBV_ILN_90 GBV_ILN_95 GBV_ILN_100 GBV_ILN_101 GBV_ILN_105 GBV_ILN_110 GBV_ILN_120 GBV_ILN_138 GBV_ILN_150 GBV_ILN_151 GBV_ILN_152 GBV_ILN_161 GBV_ILN_170 GBV_ILN_171 GBV_ILN_187 GBV_ILN_213 GBV_ILN_224 GBV_ILN_230 GBV_ILN_250 GBV_ILN_281 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_636 GBV_ILN_702 GBV_ILN_2001 GBV_ILN_2003 GBV_ILN_2004 GBV_ILN_2005 GBV_ILN_2006 GBV_ILN_2007 GBV_ILN_2008 GBV_ILN_2009 GBV_ILN_2010 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_2025 GBV_ILN_2026 GBV_ILN_2027 GBV_ILN_2031 GBV_ILN_2034 GBV_ILN_2037 GBV_ILN_2038 GBV_ILN_2039 GBV_ILN_2044 GBV_ILN_2048 GBV_ILN_2049 GBV_ILN_2050 GBV_ILN_2055 GBV_ILN_2057 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 GBV_ILN_2070 GBV_ILN_2086 GBV_ILN_2088 GBV_ILN_2093 GBV_ILN_2106 GBV_ILN_2107 GBV_ILN_2108 GBV_ILN_2110 GBV_ILN_2111 GBV_ILN_2112 GBV_ILN_2113 GBV_ILN_2116 GBV_ILN_2118 GBV_ILN_2119 GBV_ILN_2122 GBV_ILN_2129 GBV_ILN_2143 GBV_ILN_2144 GBV_ILN_2147 GBV_ILN_2148 GBV_ILN_2152 GBV_ILN_2153 GBV_ILN_2188 GBV_ILN_2190 GBV_ILN_2232 GBV_ILN_2336 GBV_ILN_2446 GBV_ILN_2470 GBV_ILN_2472 GBV_ILN_2507 GBV_ILN_2522 GBV_ILN_2548 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4046 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4242 GBV_ILN_4246 GBV_ILN_4249 GBV_ILN_4251 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4326 GBV_ILN_4333 GBV_ILN_4334 GBV_ILN_4335 GBV_ILN_4336 GBV_ILN_4338 GBV_ILN_4393 GBV_ILN_4700 AR 13 2019 5 09 838-841 |
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10.1134/S1990793119050038 doi (DE-627)SPR022589910 (SPR)S1990793119050038-e DE-627 ger DE-627 rakwb eng Korneeva, N. V. verfasserin aut Effect of the Matrix on the Properties of Carbon Fiber Reinforced Plastics 2019 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier © Pleiades Publishing, Ltd. 2019 Abstract The effect of rigid and flexible matrices on the properties of carbon fiber reinforced plastics has been studied using the impact break method at different rates of loading the composite material (CM). It has been established that the strain of CM under static loading conditions has a smooth character and is generally tensile. For this reason, CM with a plastic matrix under static loading conditions has higher properties, such as the maximum specific absorbed-in-fracture energy α = 154 J/$ cm^{2} $ and the maximum strength σ = 524 MPa at a greater relative strain ε = 6%. The fracture mechanism of carbon fiber reinforced plastics (CFRPs) abruptly changes upon an impact. The fracture of CMs is initiated by an impact at the first moment of its action. The entire process of CM strain until fracture is accompanied by fiber filament breaks. Load fluctuations occur due to filament breaks and are reflected in the strain curves in the form of peaks. The processes of filament break and crush are superimposed on the overall process of multistage CM tensile strain at a higher level. The accumulation of fiber crushes and breaks decreases the strength of CMs. This leads to fast fracture at lower strain in comparison with the case of static loading conditions. The specific absorbed-in-fracture energy α of CFRPs with a flexible matrix decreases upon an impact by a factor of 3.4, from 154 to 45 J/$ cm^{2} $, relative to the specific absorbed-in-fracture energy of CM in the static case; the material is fractured at a smaller relative strain ε = 1.7% and a lower strength σ = 496 MPa. Kudinov, V. V. aut Krylov, I. K. aut Mamonov, V. I. aut Enthalten in Russian journal of physical chemistry Moscow : MAIK Nauka, Interperiodica Publ., 2007 13(2019), 5 vom: Sept., Seite 838-841 (DE-627)688079938 (DE-600)2653166-5 1990-7923 nnns volume:13 year:2019 number:5 month:09 pages:838-841 https://dx.doi.org/10.1134/S1990793119050038 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_SPRINGER SSG-OLC-PHA GBV_ILN_11 GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_32 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_74 GBV_ILN_90 GBV_ILN_95 GBV_ILN_100 GBV_ILN_101 GBV_ILN_105 GBV_ILN_110 GBV_ILN_120 GBV_ILN_138 GBV_ILN_150 GBV_ILN_151 GBV_ILN_152 GBV_ILN_161 GBV_ILN_170 GBV_ILN_171 GBV_ILN_187 GBV_ILN_213 GBV_ILN_224 GBV_ILN_230 GBV_ILN_250 GBV_ILN_281 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_636 GBV_ILN_702 GBV_ILN_2001 GBV_ILN_2003 GBV_ILN_2004 GBV_ILN_2005 GBV_ILN_2006 GBV_ILN_2007 GBV_ILN_2008 GBV_ILN_2009 GBV_ILN_2010 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_2025 GBV_ILN_2026 GBV_ILN_2027 GBV_ILN_2031 GBV_ILN_2034 GBV_ILN_2037 GBV_ILN_2038 GBV_ILN_2039 GBV_ILN_2044 GBV_ILN_2048 GBV_ILN_2049 GBV_ILN_2050 GBV_ILN_2055 GBV_ILN_2057 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 GBV_ILN_2070 GBV_ILN_2086 GBV_ILN_2088 GBV_ILN_2093 GBV_ILN_2106 GBV_ILN_2107 GBV_ILN_2108 GBV_ILN_2110 GBV_ILN_2111 GBV_ILN_2112 GBV_ILN_2113 GBV_ILN_2116 GBV_ILN_2118 GBV_ILN_2119 GBV_ILN_2122 GBV_ILN_2129 GBV_ILN_2143 GBV_ILN_2144 GBV_ILN_2147 GBV_ILN_2148 GBV_ILN_2152 GBV_ILN_2153 GBV_ILN_2188 GBV_ILN_2190 GBV_ILN_2232 GBV_ILN_2336 GBV_ILN_2446 GBV_ILN_2470 GBV_ILN_2472 GBV_ILN_2507 GBV_ILN_2522 GBV_ILN_2548 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4046 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4242 GBV_ILN_4246 GBV_ILN_4249 GBV_ILN_4251 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4326 GBV_ILN_4333 GBV_ILN_4334 GBV_ILN_4335 GBV_ILN_4336 GBV_ILN_4338 GBV_ILN_4393 GBV_ILN_4700 AR 13 2019 5 09 838-841 |
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10.1134/S1990793119050038 doi (DE-627)SPR022589910 (SPR)S1990793119050038-e DE-627 ger DE-627 rakwb eng Korneeva, N. V. verfasserin aut Effect of the Matrix on the Properties of Carbon Fiber Reinforced Plastics 2019 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier © Pleiades Publishing, Ltd. 2019 Abstract The effect of rigid and flexible matrices on the properties of carbon fiber reinforced plastics has been studied using the impact break method at different rates of loading the composite material (CM). It has been established that the strain of CM under static loading conditions has a smooth character and is generally tensile. For this reason, CM with a plastic matrix under static loading conditions has higher properties, such as the maximum specific absorbed-in-fracture energy α = 154 J/$ cm^{2} $ and the maximum strength σ = 524 MPa at a greater relative strain ε = 6%. The fracture mechanism of carbon fiber reinforced plastics (CFRPs) abruptly changes upon an impact. The fracture of CMs is initiated by an impact at the first moment of its action. The entire process of CM strain until fracture is accompanied by fiber filament breaks. Load fluctuations occur due to filament breaks and are reflected in the strain curves in the form of peaks. The processes of filament break and crush are superimposed on the overall process of multistage CM tensile strain at a higher level. The accumulation of fiber crushes and breaks decreases the strength of CMs. This leads to fast fracture at lower strain in comparison with the case of static loading conditions. The specific absorbed-in-fracture energy α of CFRPs with a flexible matrix decreases upon an impact by a factor of 3.4, from 154 to 45 J/$ cm^{2} $, relative to the specific absorbed-in-fracture energy of CM in the static case; the material is fractured at a smaller relative strain ε = 1.7% and a lower strength σ = 496 MPa. Kudinov, V. V. aut Krylov, I. K. aut Mamonov, V. I. aut Enthalten in Russian journal of physical chemistry Moscow : MAIK Nauka, Interperiodica Publ., 2007 13(2019), 5 vom: Sept., Seite 838-841 (DE-627)688079938 (DE-600)2653166-5 1990-7923 nnns volume:13 year:2019 number:5 month:09 pages:838-841 https://dx.doi.org/10.1134/S1990793119050038 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_SPRINGER SSG-OLC-PHA GBV_ILN_11 GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_32 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_74 GBV_ILN_90 GBV_ILN_95 GBV_ILN_100 GBV_ILN_101 GBV_ILN_105 GBV_ILN_110 GBV_ILN_120 GBV_ILN_138 GBV_ILN_150 GBV_ILN_151 GBV_ILN_152 GBV_ILN_161 GBV_ILN_170 GBV_ILN_171 GBV_ILN_187 GBV_ILN_213 GBV_ILN_224 GBV_ILN_230 GBV_ILN_250 GBV_ILN_281 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_636 GBV_ILN_702 GBV_ILN_2001 GBV_ILN_2003 GBV_ILN_2004 GBV_ILN_2005 GBV_ILN_2006 GBV_ILN_2007 GBV_ILN_2008 GBV_ILN_2009 GBV_ILN_2010 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_2025 GBV_ILN_2026 GBV_ILN_2027 GBV_ILN_2031 GBV_ILN_2034 GBV_ILN_2037 GBV_ILN_2038 GBV_ILN_2039 GBV_ILN_2044 GBV_ILN_2048 GBV_ILN_2049 GBV_ILN_2050 GBV_ILN_2055 GBV_ILN_2057 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 GBV_ILN_2070 GBV_ILN_2086 GBV_ILN_2088 GBV_ILN_2093 GBV_ILN_2106 GBV_ILN_2107 GBV_ILN_2108 GBV_ILN_2110 GBV_ILN_2111 GBV_ILN_2112 GBV_ILN_2113 GBV_ILN_2116 GBV_ILN_2118 GBV_ILN_2119 GBV_ILN_2122 GBV_ILN_2129 GBV_ILN_2143 GBV_ILN_2144 GBV_ILN_2147 GBV_ILN_2148 GBV_ILN_2152 GBV_ILN_2153 GBV_ILN_2188 GBV_ILN_2190 GBV_ILN_2232 GBV_ILN_2336 GBV_ILN_2446 GBV_ILN_2470 GBV_ILN_2472 GBV_ILN_2507 GBV_ILN_2522 GBV_ILN_2548 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4046 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4242 GBV_ILN_4246 GBV_ILN_4249 GBV_ILN_4251 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4326 GBV_ILN_4333 GBV_ILN_4334 GBV_ILN_4335 GBV_ILN_4336 GBV_ILN_4338 GBV_ILN_4393 GBV_ILN_4700 AR 13 2019 5 09 838-841 |
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Korneeva, N. V. @@aut@@ Kudinov, V. V. @@aut@@ Krylov, I. K. @@aut@@ Mamonov, V. I. @@aut@@ |
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It has been established that the strain of CM under static loading conditions has a smooth character and is generally tensile. For this reason, CM with a plastic matrix under static loading conditions has higher properties, such as the maximum specific absorbed-in-fracture energy α = 154 J/$ cm^{2} $ and the maximum strength σ = 524 MPa at a greater relative strain ε = 6%. The fracture mechanism of carbon fiber reinforced plastics (CFRPs) abruptly changes upon an impact. The fracture of CMs is initiated by an impact at the first moment of its action. The entire process of CM strain until fracture is accompanied by fiber filament breaks. Load fluctuations occur due to filament breaks and are reflected in the strain curves in the form of peaks. The processes of filament break and crush are superimposed on the overall process of multistage CM tensile strain at a higher level. 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Korneeva, N. V. |
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Korneeva, N. V. Effect of the Matrix on the Properties of Carbon Fiber Reinforced Plastics |
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Effect of the Matrix on the Properties of Carbon Fiber Reinforced Plastics |
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Effect of the Matrix on the Properties of Carbon Fiber Reinforced Plastics |
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Korneeva, N. V. |
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10.1134/S1990793119050038 |
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effect of the matrix on the properties of carbon fiber reinforced plastics |
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Effect of the Matrix on the Properties of Carbon Fiber Reinforced Plastics |
| abstract |
Abstract The effect of rigid and flexible matrices on the properties of carbon fiber reinforced plastics has been studied using the impact break method at different rates of loading the composite material (CM). It has been established that the strain of CM under static loading conditions has a smooth character and is generally tensile. For this reason, CM with a plastic matrix under static loading conditions has higher properties, such as the maximum specific absorbed-in-fracture energy α = 154 J/$ cm^{2} $ and the maximum strength σ = 524 MPa at a greater relative strain ε = 6%. The fracture mechanism of carbon fiber reinforced plastics (CFRPs) abruptly changes upon an impact. The fracture of CMs is initiated by an impact at the first moment of its action. The entire process of CM strain until fracture is accompanied by fiber filament breaks. Load fluctuations occur due to filament breaks and are reflected in the strain curves in the form of peaks. The processes of filament break and crush are superimposed on the overall process of multistage CM tensile strain at a higher level. The accumulation of fiber crushes and breaks decreases the strength of CMs. This leads to fast fracture at lower strain in comparison with the case of static loading conditions. The specific absorbed-in-fracture energy α of CFRPs with a flexible matrix decreases upon an impact by a factor of 3.4, from 154 to 45 J/$ cm^{2} $, relative to the specific absorbed-in-fracture energy of CM in the static case; the material is fractured at a smaller relative strain ε = 1.7% and a lower strength σ = 496 MPa. © Pleiades Publishing, Ltd. 2019 |
| abstractGer |
Abstract The effect of rigid and flexible matrices on the properties of carbon fiber reinforced plastics has been studied using the impact break method at different rates of loading the composite material (CM). It has been established that the strain of CM under static loading conditions has a smooth character and is generally tensile. For this reason, CM with a plastic matrix under static loading conditions has higher properties, such as the maximum specific absorbed-in-fracture energy α = 154 J/$ cm^{2} $ and the maximum strength σ = 524 MPa at a greater relative strain ε = 6%. The fracture mechanism of carbon fiber reinforced plastics (CFRPs) abruptly changes upon an impact. The fracture of CMs is initiated by an impact at the first moment of its action. The entire process of CM strain until fracture is accompanied by fiber filament breaks. Load fluctuations occur due to filament breaks and are reflected in the strain curves in the form of peaks. The processes of filament break and crush are superimposed on the overall process of multistage CM tensile strain at a higher level. The accumulation of fiber crushes and breaks decreases the strength of CMs. This leads to fast fracture at lower strain in comparison with the case of static loading conditions. The specific absorbed-in-fracture energy α of CFRPs with a flexible matrix decreases upon an impact by a factor of 3.4, from 154 to 45 J/$ cm^{2} $, relative to the specific absorbed-in-fracture energy of CM in the static case; the material is fractured at a smaller relative strain ε = 1.7% and a lower strength σ = 496 MPa. © Pleiades Publishing, Ltd. 2019 |
| abstract_unstemmed |
Abstract The effect of rigid and flexible matrices on the properties of carbon fiber reinforced plastics has been studied using the impact break method at different rates of loading the composite material (CM). It has been established that the strain of CM under static loading conditions has a smooth character and is generally tensile. For this reason, CM with a plastic matrix under static loading conditions has higher properties, such as the maximum specific absorbed-in-fracture energy α = 154 J/$ cm^{2} $ and the maximum strength σ = 524 MPa at a greater relative strain ε = 6%. The fracture mechanism of carbon fiber reinforced plastics (CFRPs) abruptly changes upon an impact. The fracture of CMs is initiated by an impact at the first moment of its action. The entire process of CM strain until fracture is accompanied by fiber filament breaks. Load fluctuations occur due to filament breaks and are reflected in the strain curves in the form of peaks. The processes of filament break and crush are superimposed on the overall process of multistage CM tensile strain at a higher level. The accumulation of fiber crushes and breaks decreases the strength of CMs. This leads to fast fracture at lower strain in comparison with the case of static loading conditions. The specific absorbed-in-fracture energy α of CFRPs with a flexible matrix decreases upon an impact by a factor of 3.4, from 154 to 45 J/$ cm^{2} $, relative to the specific absorbed-in-fracture energy of CM in the static case; the material is fractured at a smaller relative strain ε = 1.7% and a lower strength σ = 496 MPa. © Pleiades Publishing, Ltd. 2019 |
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Effect of the Matrix on the Properties of Carbon Fiber Reinforced Plastics |
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https://dx.doi.org/10.1134/S1990793119050038 |
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Kudinov, V. V. Krylov, I. K. Mamonov, V. I. |
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Kudinov, V. V. Krylov, I. K. Mamonov, V. I. |
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10.1134/S1990793119050038 |
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2024-07-03T13:52:20.768Z |
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| score |
7.4013176 |