High Strain-Rate Through-Thickness Compression Testing of Symmetrical Inter-ply Hybrid Polymer Composites Reinforced with Carbon/Glass and Carbon/Kevlar Fibers
Abstract A compressive split Hopkinson pressure bar (SHPB) apparatus is utilised for the high strain-rate investigation of symmetrical epoxy-based carbon/glass (CGE) and carbon/Kevlar (CKE) hybrid composite samples along the through-thickness direction. The stacking sequence used for the hybrid comp...
Ausführliche Beschreibung
Gespeichert in:
| Autor*in: |
Prusty, Rajesh Kumar [verfasserIn] |
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| Format: |
E-Artikel |
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| Sprache: |
Englisch |
| Erschienen: |
2022 |
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| Schlagwörter: |
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| Anmerkung: |
© The Indian Institute of Metals - IIM 2022 |
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| Übergeordnetes Werk: |
Enthalten in: Transactions of the Indian Institute of Metals - [New Delhi] : Springer India, 2008, 75(2022), 10 vom: 19. Mai, Seite 2507-2516 |
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| Übergeordnetes Werk: |
volume:75 ; year:2022 ; number:10 ; day:19 ; month:05 ; pages:2507-2516 |
| Links: |
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| DOI / URN: |
10.1007/s12666-022-02619-0 |
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| Katalog-ID: |
SPR048314005 |
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| 520 | |a Abstract A compressive split Hopkinson pressure bar (SHPB) apparatus is utilised for the high strain-rate investigation of symmetrical epoxy-based carbon/glass (CGE) and carbon/Kevlar (CKE) hybrid composite samples along the through-thickness direction. The stacking sequence used for the hybrid composites was [$ C_{5} $/$ G_{5} $]S and [$ C_{5} $/$ K_{5} $]S. Compared to the density of neat epoxy-based carbon (CE) composite, the density of CGE composite was about 14% higher, whereas the density of CKE composite was about 8% lower. An initial striker velocity of about 25 m/s was used for all experiments. The mean reference strain rate observed for CGE and CKE hybrid composites was 2293 and 2333 $ s^{−1} $, respectively, with a negligible difference in mean compressive strength. The mean strain to failure of [$ C_{5} $/$ K_{5} $]S was almost 17% higher than [$ C_{5} $/$ G_{5} $]S, and proper stress equilibrium was observed. This article presents the significant outcomes of SHPB testing, including mechanical response and failure analysis of the hybrid composite samples. | ||
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| 650 | 4 | |a Fiber-reinforced polymer |7 (dpeaa)DE-He213 | |
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| 650 | 4 | |a High strain rate |7 (dpeaa)DE-He213 | |
| 700 | 1 | |a Ray, Bankim Chandra |4 aut | |
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10.1007/s12666-022-02619-0 doi (DE-627)SPR048314005 (SPR)s12666-022-02619-0-e DE-627 ger DE-627 rakwb eng Prusty, Rajesh Kumar verfasserin aut High Strain-Rate Through-Thickness Compression Testing of Symmetrical Inter-ply Hybrid Polymer Composites Reinforced with Carbon/Glass and Carbon/Kevlar Fibers 2022 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier © The Indian Institute of Metals - IIM 2022 Abstract A compressive split Hopkinson pressure bar (SHPB) apparatus is utilised for the high strain-rate investigation of symmetrical epoxy-based carbon/glass (CGE) and carbon/Kevlar (CKE) hybrid composite samples along the through-thickness direction. The stacking sequence used for the hybrid composites was [$ C_{5} $/$ G_{5} $]S and [$ C_{5} $/$ K_{5} $]S. Compared to the density of neat epoxy-based carbon (CE) composite, the density of CGE composite was about 14% higher, whereas the density of CKE composite was about 8% lower. An initial striker velocity of about 25 m/s was used for all experiments. The mean reference strain rate observed for CGE and CKE hybrid composites was 2293 and 2333 $ s^{−1} $, respectively, with a negligible difference in mean compressive strength. The mean strain to failure of [$ C_{5} $/$ K_{5} $]S was almost 17% higher than [$ C_{5} $/$ G_{5} $]S, and proper stress equilibrium was observed. This article presents the significant outcomes of SHPB testing, including mechanical response and failure analysis of the hybrid composite samples. Split Hopkinson pressure bar (dpeaa)DE-He213 Fiber-reinforced polymer (dpeaa)DE-He213 Hybrid composite (dpeaa)DE-He213 High strain rate (dpeaa)DE-He213 Ray, Bankim Chandra aut Enthalten in Transactions of the Indian Institute of Metals [New Delhi] : Springer India, 2008 75(2022), 10 vom: 19. Mai, Seite 2507-2516 (DE-627)617807884 (DE-600)2535335-4 0975-1645 nnns volume:75 year:2022 number:10 day:19 month:05 pages:2507-2516 https://dx.doi.org/10.1007/s12666-022-02619-0 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_SPRINGER 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_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_2056 GBV_ILN_2057 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 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_2118 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_4126 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_4328 GBV_ILN_4333 GBV_ILN_4334 GBV_ILN_4335 GBV_ILN_4336 GBV_ILN_4338 GBV_ILN_4393 GBV_ILN_4700 AR 75 2022 10 19 05 2507-2516 |
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10.1007/s12666-022-02619-0 doi (DE-627)SPR048314005 (SPR)s12666-022-02619-0-e DE-627 ger DE-627 rakwb eng Prusty, Rajesh Kumar verfasserin aut High Strain-Rate Through-Thickness Compression Testing of Symmetrical Inter-ply Hybrid Polymer Composites Reinforced with Carbon/Glass and Carbon/Kevlar Fibers 2022 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier © The Indian Institute of Metals - IIM 2022 Abstract A compressive split Hopkinson pressure bar (SHPB) apparatus is utilised for the high strain-rate investigation of symmetrical epoxy-based carbon/glass (CGE) and carbon/Kevlar (CKE) hybrid composite samples along the through-thickness direction. The stacking sequence used for the hybrid composites was [$ C_{5} $/$ G_{5} $]S and [$ C_{5} $/$ K_{5} $]S. Compared to the density of neat epoxy-based carbon (CE) composite, the density of CGE composite was about 14% higher, whereas the density of CKE composite was about 8% lower. An initial striker velocity of about 25 m/s was used for all experiments. The mean reference strain rate observed for CGE and CKE hybrid composites was 2293 and 2333 $ s^{−1} $, respectively, with a negligible difference in mean compressive strength. The mean strain to failure of [$ C_{5} $/$ K_{5} $]S was almost 17% higher than [$ C_{5} $/$ G_{5} $]S, and proper stress equilibrium was observed. This article presents the significant outcomes of SHPB testing, including mechanical response and failure analysis of the hybrid composite samples. Split Hopkinson pressure bar (dpeaa)DE-He213 Fiber-reinforced polymer (dpeaa)DE-He213 Hybrid composite (dpeaa)DE-He213 High strain rate (dpeaa)DE-He213 Ray, Bankim Chandra aut Enthalten in Transactions of the Indian Institute of Metals [New Delhi] : Springer India, 2008 75(2022), 10 vom: 19. Mai, Seite 2507-2516 (DE-627)617807884 (DE-600)2535335-4 0975-1645 nnns volume:75 year:2022 number:10 day:19 month:05 pages:2507-2516 https://dx.doi.org/10.1007/s12666-022-02619-0 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_SPRINGER 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_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_2056 GBV_ILN_2057 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 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_2118 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_4126 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_4328 GBV_ILN_4333 GBV_ILN_4334 GBV_ILN_4335 GBV_ILN_4336 GBV_ILN_4338 GBV_ILN_4393 GBV_ILN_4700 AR 75 2022 10 19 05 2507-2516 |
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10.1007/s12666-022-02619-0 doi (DE-627)SPR048314005 (SPR)s12666-022-02619-0-e DE-627 ger DE-627 rakwb eng Prusty, Rajesh Kumar verfasserin aut High Strain-Rate Through-Thickness Compression Testing of Symmetrical Inter-ply Hybrid Polymer Composites Reinforced with Carbon/Glass and Carbon/Kevlar Fibers 2022 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier © The Indian Institute of Metals - IIM 2022 Abstract A compressive split Hopkinson pressure bar (SHPB) apparatus is utilised for the high strain-rate investigation of symmetrical epoxy-based carbon/glass (CGE) and carbon/Kevlar (CKE) hybrid composite samples along the through-thickness direction. The stacking sequence used for the hybrid composites was [$ C_{5} $/$ G_{5} $]S and [$ C_{5} $/$ K_{5} $]S. Compared to the density of neat epoxy-based carbon (CE) composite, the density of CGE composite was about 14% higher, whereas the density of CKE composite was about 8% lower. An initial striker velocity of about 25 m/s was used for all experiments. The mean reference strain rate observed for CGE and CKE hybrid composites was 2293 and 2333 $ s^{−1} $, respectively, with a negligible difference in mean compressive strength. The mean strain to failure of [$ C_{5} $/$ K_{5} $]S was almost 17% higher than [$ C_{5} $/$ G_{5} $]S, and proper stress equilibrium was observed. This article presents the significant outcomes of SHPB testing, including mechanical response and failure analysis of the hybrid composite samples. Split Hopkinson pressure bar (dpeaa)DE-He213 Fiber-reinforced polymer (dpeaa)DE-He213 Hybrid composite (dpeaa)DE-He213 High strain rate (dpeaa)DE-He213 Ray, Bankim Chandra aut Enthalten in Transactions of the Indian Institute of Metals [New Delhi] : Springer India, 2008 75(2022), 10 vom: 19. Mai, Seite 2507-2516 (DE-627)617807884 (DE-600)2535335-4 0975-1645 nnns volume:75 year:2022 number:10 day:19 month:05 pages:2507-2516 https://dx.doi.org/10.1007/s12666-022-02619-0 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_SPRINGER 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_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_2056 GBV_ILN_2057 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 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_2118 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_4126 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_4328 GBV_ILN_4333 GBV_ILN_4334 GBV_ILN_4335 GBV_ILN_4336 GBV_ILN_4338 GBV_ILN_4393 GBV_ILN_4700 AR 75 2022 10 19 05 2507-2516 |
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10.1007/s12666-022-02619-0 doi (DE-627)SPR048314005 (SPR)s12666-022-02619-0-e DE-627 ger DE-627 rakwb eng Prusty, Rajesh Kumar verfasserin aut High Strain-Rate Through-Thickness Compression Testing of Symmetrical Inter-ply Hybrid Polymer Composites Reinforced with Carbon/Glass and Carbon/Kevlar Fibers 2022 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier © The Indian Institute of Metals - IIM 2022 Abstract A compressive split Hopkinson pressure bar (SHPB) apparatus is utilised for the high strain-rate investigation of symmetrical epoxy-based carbon/glass (CGE) and carbon/Kevlar (CKE) hybrid composite samples along the through-thickness direction. The stacking sequence used for the hybrid composites was [$ C_{5} $/$ G_{5} $]S and [$ C_{5} $/$ K_{5} $]S. Compared to the density of neat epoxy-based carbon (CE) composite, the density of CGE composite was about 14% higher, whereas the density of CKE composite was about 8% lower. An initial striker velocity of about 25 m/s was used for all experiments. The mean reference strain rate observed for CGE and CKE hybrid composites was 2293 and 2333 $ s^{−1} $, respectively, with a negligible difference in mean compressive strength. The mean strain to failure of [$ C_{5} $/$ K_{5} $]S was almost 17% higher than [$ C_{5} $/$ G_{5} $]S, and proper stress equilibrium was observed. This article presents the significant outcomes of SHPB testing, including mechanical response and failure analysis of the hybrid composite samples. Split Hopkinson pressure bar (dpeaa)DE-He213 Fiber-reinforced polymer (dpeaa)DE-He213 Hybrid composite (dpeaa)DE-He213 High strain rate (dpeaa)DE-He213 Ray, Bankim Chandra aut Enthalten in Transactions of the Indian Institute of Metals [New Delhi] : Springer India, 2008 75(2022), 10 vom: 19. Mai, Seite 2507-2516 (DE-627)617807884 (DE-600)2535335-4 0975-1645 nnns volume:75 year:2022 number:10 day:19 month:05 pages:2507-2516 https://dx.doi.org/10.1007/s12666-022-02619-0 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_SPRINGER 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_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_2056 GBV_ILN_2057 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 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_2118 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_4126 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_4328 GBV_ILN_4333 GBV_ILN_4334 GBV_ILN_4335 GBV_ILN_4336 GBV_ILN_4338 GBV_ILN_4393 GBV_ILN_4700 AR 75 2022 10 19 05 2507-2516 |
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10.1007/s12666-022-02619-0 doi (DE-627)SPR048314005 (SPR)s12666-022-02619-0-e DE-627 ger DE-627 rakwb eng Prusty, Rajesh Kumar verfasserin aut High Strain-Rate Through-Thickness Compression Testing of Symmetrical Inter-ply Hybrid Polymer Composites Reinforced with Carbon/Glass and Carbon/Kevlar Fibers 2022 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier © The Indian Institute of Metals - IIM 2022 Abstract A compressive split Hopkinson pressure bar (SHPB) apparatus is utilised for the high strain-rate investigation of symmetrical epoxy-based carbon/glass (CGE) and carbon/Kevlar (CKE) hybrid composite samples along the through-thickness direction. The stacking sequence used for the hybrid composites was [$ C_{5} $/$ G_{5} $]S and [$ C_{5} $/$ K_{5} $]S. Compared to the density of neat epoxy-based carbon (CE) composite, the density of CGE composite was about 14% higher, whereas the density of CKE composite was about 8% lower. An initial striker velocity of about 25 m/s was used for all experiments. The mean reference strain rate observed for CGE and CKE hybrid composites was 2293 and 2333 $ s^{−1} $, respectively, with a negligible difference in mean compressive strength. The mean strain to failure of [$ C_{5} $/$ K_{5} $]S was almost 17% higher than [$ C_{5} $/$ G_{5} $]S, and proper stress equilibrium was observed. This article presents the significant outcomes of SHPB testing, including mechanical response and failure analysis of the hybrid composite samples. Split Hopkinson pressure bar (dpeaa)DE-He213 Fiber-reinforced polymer (dpeaa)DE-He213 Hybrid composite (dpeaa)DE-He213 High strain rate (dpeaa)DE-He213 Ray, Bankim Chandra aut Enthalten in Transactions of the Indian Institute of Metals [New Delhi] : Springer India, 2008 75(2022), 10 vom: 19. Mai, Seite 2507-2516 (DE-627)617807884 (DE-600)2535335-4 0975-1645 nnns volume:75 year:2022 number:10 day:19 month:05 pages:2507-2516 https://dx.doi.org/10.1007/s12666-022-02619-0 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_SPRINGER 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_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_2056 GBV_ILN_2057 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 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_2118 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_4126 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_4328 GBV_ILN_4333 GBV_ILN_4334 GBV_ILN_4335 GBV_ILN_4336 GBV_ILN_4338 GBV_ILN_4393 GBV_ILN_4700 AR 75 2022 10 19 05 2507-2516 |
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The stacking sequence used for the hybrid composites was [$ C_{5} $/$ G_{5} $]S and [$ C_{5} $/$ K_{5} $]S. Compared to the density of neat epoxy-based carbon (CE) composite, the density of CGE composite was about 14% higher, whereas the density of CKE composite was about 8% lower. An initial striker velocity of about 25 m/s was used for all experiments. The mean reference strain rate observed for CGE and CKE hybrid composites was 2293 and 2333 $ s^{−1} $, respectively, with a negligible difference in mean compressive strength. The mean strain to failure of [$ C_{5} $/$ K_{5} $]S was almost 17% higher than [$ C_{5} $/$ G_{5} $]S, and proper stress equilibrium was observed. 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| author |
Prusty, Rajesh Kumar |
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Prusty, Rajesh Kumar misc Split Hopkinson pressure bar misc Fiber-reinforced polymer misc Hybrid composite misc High strain rate High Strain-Rate Through-Thickness Compression Testing of Symmetrical Inter-ply Hybrid Polymer Composites Reinforced with Carbon/Glass and Carbon/Kevlar Fibers |
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High Strain-Rate Through-Thickness Compression Testing of Symmetrical Inter-ply Hybrid Polymer Composites Reinforced with Carbon/Glass and Carbon/Kevlar Fibers Split Hopkinson pressure bar (dpeaa)DE-He213 Fiber-reinforced polymer (dpeaa)DE-He213 Hybrid composite (dpeaa)DE-He213 High strain rate (dpeaa)DE-He213 |
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misc Split Hopkinson pressure bar misc Fiber-reinforced polymer misc Hybrid composite misc High strain rate |
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misc Split Hopkinson pressure bar misc Fiber-reinforced polymer misc Hybrid composite misc High strain rate |
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High Strain-Rate Through-Thickness Compression Testing of Symmetrical Inter-ply Hybrid Polymer Composites Reinforced with Carbon/Glass and Carbon/Kevlar Fibers |
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High Strain-Rate Through-Thickness Compression Testing of Symmetrical Inter-ply Hybrid Polymer Composites Reinforced with Carbon/Glass and Carbon/Kevlar Fibers |
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Prusty, Rajesh Kumar |
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Prusty, Rajesh Kumar Ray, Bankim Chandra |
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Elektronische Aufsätze |
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Prusty, Rajesh Kumar |
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10.1007/s12666-022-02619-0 |
| title_sort |
high strain-rate through-thickness compression testing of symmetrical inter-ply hybrid polymer composites reinforced with carbon/glass and carbon/kevlar fibers |
| title_auth |
High Strain-Rate Through-Thickness Compression Testing of Symmetrical Inter-ply Hybrid Polymer Composites Reinforced with Carbon/Glass and Carbon/Kevlar Fibers |
| abstract |
Abstract A compressive split Hopkinson pressure bar (SHPB) apparatus is utilised for the high strain-rate investigation of symmetrical epoxy-based carbon/glass (CGE) and carbon/Kevlar (CKE) hybrid composite samples along the through-thickness direction. The stacking sequence used for the hybrid composites was [$ C_{5} $/$ G_{5} $]S and [$ C_{5} $/$ K_{5} $]S. Compared to the density of neat epoxy-based carbon (CE) composite, the density of CGE composite was about 14% higher, whereas the density of CKE composite was about 8% lower. An initial striker velocity of about 25 m/s was used for all experiments. The mean reference strain rate observed for CGE and CKE hybrid composites was 2293 and 2333 $ s^{−1} $, respectively, with a negligible difference in mean compressive strength. The mean strain to failure of [$ C_{5} $/$ K_{5} $]S was almost 17% higher than [$ C_{5} $/$ G_{5} $]S, and proper stress equilibrium was observed. This article presents the significant outcomes of SHPB testing, including mechanical response and failure analysis of the hybrid composite samples. © The Indian Institute of Metals - IIM 2022 |
| abstractGer |
Abstract A compressive split Hopkinson pressure bar (SHPB) apparatus is utilised for the high strain-rate investigation of symmetrical epoxy-based carbon/glass (CGE) and carbon/Kevlar (CKE) hybrid composite samples along the through-thickness direction. The stacking sequence used for the hybrid composites was [$ C_{5} $/$ G_{5} $]S and [$ C_{5} $/$ K_{5} $]S. Compared to the density of neat epoxy-based carbon (CE) composite, the density of CGE composite was about 14% higher, whereas the density of CKE composite was about 8% lower. An initial striker velocity of about 25 m/s was used for all experiments. The mean reference strain rate observed for CGE and CKE hybrid composites was 2293 and 2333 $ s^{−1} $, respectively, with a negligible difference in mean compressive strength. The mean strain to failure of [$ C_{5} $/$ K_{5} $]S was almost 17% higher than [$ C_{5} $/$ G_{5} $]S, and proper stress equilibrium was observed. This article presents the significant outcomes of SHPB testing, including mechanical response and failure analysis of the hybrid composite samples. © The Indian Institute of Metals - IIM 2022 |
| abstract_unstemmed |
Abstract A compressive split Hopkinson pressure bar (SHPB) apparatus is utilised for the high strain-rate investigation of symmetrical epoxy-based carbon/glass (CGE) and carbon/Kevlar (CKE) hybrid composite samples along the through-thickness direction. The stacking sequence used for the hybrid composites was [$ C_{5} $/$ G_{5} $]S and [$ C_{5} $/$ K_{5} $]S. Compared to the density of neat epoxy-based carbon (CE) composite, the density of CGE composite was about 14% higher, whereas the density of CKE composite was about 8% lower. An initial striker velocity of about 25 m/s was used for all experiments. The mean reference strain rate observed for CGE and CKE hybrid composites was 2293 and 2333 $ s^{−1} $, respectively, with a negligible difference in mean compressive strength. The mean strain to failure of [$ C_{5} $/$ K_{5} $]S was almost 17% higher than [$ C_{5} $/$ G_{5} $]S, and proper stress equilibrium was observed. This article presents the significant outcomes of SHPB testing, including mechanical response and failure analysis of the hybrid composite samples. © The Indian Institute of Metals - IIM 2022 |
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High Strain-Rate Through-Thickness Compression Testing of Symmetrical Inter-ply Hybrid Polymer Composites Reinforced with Carbon/Glass and Carbon/Kevlar Fibers |
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https://dx.doi.org/10.1007/s12666-022-02619-0 |
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Ray, Bankim Chandra |
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10.1007/s12666-022-02619-0 |
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2024-07-03T18:24:42.866Z |
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