Experimental and numerical characterization of tensile property of jute/carbon fabric reinforced epoxy hybrid composites

Abstract Jute based green composites are emerging materials due to their certain attractive properties like appropriate strength to weight ratio, high damping ratio, low price and corrosion resistance. Jute/carbon hybrid composite can replace carbon fiber reinforced composites without much loss in t...
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Autor*in:	Khalid, Muhammad Yasir [verfasserIn] Nasir, Muhammad Ali [verfasserIn] Ali, Aakash [verfasserIn] Al Rashid, Ans [verfasserIn] Khan, Muhammad Riaz [verfasserIn]

Format:	E-Artikel
Sprache:	Englisch

Erschienen:	2020

Schlagwörter:	Hybrid composites CFRP Laminated textile composites Simulation

Übergeordnetes Werk:	Enthalten in: SN applied sciences - [Cham] : Springer International Publishing, 2019, 2(2020), 4 vom: 07. März
Übergeordnetes Werk:	volume:2 ; year:2020 ; number:4 ; day:07 ; month:03

Links:	Volltext

DOI / URN:	10.1007/s42452-020-2403-2

Katalog-ID:	SPR039030016

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245	1	0	\|a Experimental and numerical characterization of tensile property of jute/carbon fabric reinforced epoxy hybrid composites
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520			\|a Abstract Jute based green composites are emerging materials due to their certain attractive properties like appropriate strength to weight ratio, high damping ratio, low price and corrosion resistance. Jute/carbon hybrid composite can replace carbon fiber reinforced composites without much loss in tensile strength. These hybrid composites are now being used in various automobile interior and exterior parts. In this study tensile behavior of carbon/jute reinforced epoxy hybrid textile composites, for different volume fractions of carbon and jute fibers, is studied experimentally and numerically. Tensile behavior of composite materials is always required for design and analysis of any structure. It is found that with increase in jute percentage tensile strength of hybrid composite decrease. Numerical results agrees well with experimental results and error increases with increase in jute percentage due to heterogeneous jute properties and waviness of fabrics. Fractographic study reveals that delamination phenomenon exists in between plies and jute fiber shows more pullout than carbon fiber. Scanning electron microscope analysis depicted that matrix fails in form of fragmentation while fibers show pullout during failure.
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700	1		\|a Khan, Muhammad Riaz \|e verfasserin \|4 aut
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author_variant	m y k my myk m a n ma man a a aa r a a ra raa m r k mr mrk
matchkey_str	article:25233971:2020----::xeietlnnmrclhrceiainfeslpoetojtcrofbiri
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allfields	10.1007/s42452-020-2403-2 doi (DE-627)SPR039030016 (DE-599)SPRs42452-020-2403-2-e (SPR)s42452-020-2403-2-e DE-627 ger DE-627 rakwb eng 500 ASE 500 ASE 50.00 bkl 35.00 bkl 33.00 bkl Khalid, Muhammad Yasir verfasserin aut Experimental and numerical characterization of tensile property of jute/carbon fabric reinforced epoxy hybrid composites 2020 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier Abstract Jute based green composites are emerging materials due to their certain attractive properties like appropriate strength to weight ratio, high damping ratio, low price and corrosion resistance. Jute/carbon hybrid composite can replace carbon fiber reinforced composites without much loss in tensile strength. These hybrid composites are now being used in various automobile interior and exterior parts. In this study tensile behavior of carbon/jute reinforced epoxy hybrid textile composites, for different volume fractions of carbon and jute fibers, is studied experimentally and numerically. Tensile behavior of composite materials is always required for design and analysis of any structure. It is found that with increase in jute percentage tensile strength of hybrid composite decrease. Numerical results agrees well with experimental results and error increases with increase in jute percentage due to heterogeneous jute properties and waviness of fabrics. Fractographic study reveals that delamination phenomenon exists in between plies and jute fiber shows more pullout than carbon fiber. Scanning electron microscope analysis depicted that matrix fails in form of fragmentation while fibers show pullout during failure. Hybrid composites (dpeaa)DE-He213 CFRP (dpeaa)DE-He213 Laminated textile composites (dpeaa)DE-He213 Simulation (dpeaa)DE-He213 Nasir, Muhammad Ali verfasserin aut Ali, Aakash verfasserin aut Al Rashid, Ans verfasserin aut Khan, Muhammad Riaz verfasserin aut Enthalten in SN applied sciences [Cham] : Springer International Publishing, 2019 2(2020), 4 vom: 07. März (DE-627)103761139X (DE-600)2947292-1 2523-3971 nnns volume:2 year:2020 number:4 day:07 month:03 https://dx.doi.org/10.1007/s42452-020-2403-2 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_90 GBV_ILN_95 GBV_ILN_100 GBV_ILN_105 GBV_ILN_110 GBV_ILN_138 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_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_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_2190 GBV_ILN_2232 GBV_ILN_2336 GBV_ILN_2470 GBV_ILN_2472 GBV_ILN_2507 GBV_ILN_2522 GBV_ILN_4012 GBV_ILN_4035 GBV_ILN_4037 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_4367 GBV_ILN_4393 GBV_ILN_4700 50.00 ASE 35.00 ASE 33.00 ASE AR 2 2020 4 07 03
spelling	10.1007/s42452-020-2403-2 doi (DE-627)SPR039030016 (DE-599)SPRs42452-020-2403-2-e (SPR)s42452-020-2403-2-e DE-627 ger DE-627 rakwb eng 500 ASE 500 ASE 50.00 bkl 35.00 bkl 33.00 bkl Khalid, Muhammad Yasir verfasserin aut Experimental and numerical characterization of tensile property of jute/carbon fabric reinforced epoxy hybrid composites 2020 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier Abstract Jute based green composites are emerging materials due to their certain attractive properties like appropriate strength to weight ratio, high damping ratio, low price and corrosion resistance. Jute/carbon hybrid composite can replace carbon fiber reinforced composites without much loss in tensile strength. These hybrid composites are now being used in various automobile interior and exterior parts. In this study tensile behavior of carbon/jute reinforced epoxy hybrid textile composites, for different volume fractions of carbon and jute fibers, is studied experimentally and numerically. Tensile behavior of composite materials is always required for design and analysis of any structure. It is found that with increase in jute percentage tensile strength of hybrid composite decrease. Numerical results agrees well with experimental results and error increases with increase in jute percentage due to heterogeneous jute properties and waviness of fabrics. Fractographic study reveals that delamination phenomenon exists in between plies and jute fiber shows more pullout than carbon fiber. Scanning electron microscope analysis depicted that matrix fails in form of fragmentation while fibers show pullout during failure. Hybrid composites (dpeaa)DE-He213 CFRP (dpeaa)DE-He213 Laminated textile composites (dpeaa)DE-He213 Simulation (dpeaa)DE-He213 Nasir, Muhammad Ali verfasserin aut Ali, Aakash verfasserin aut Al Rashid, Ans verfasserin aut Khan, Muhammad Riaz verfasserin aut Enthalten in SN applied sciences [Cham] : Springer International Publishing, 2019 2(2020), 4 vom: 07. März (DE-627)103761139X (DE-600)2947292-1 2523-3971 nnns volume:2 year:2020 number:4 day:07 month:03 https://dx.doi.org/10.1007/s42452-020-2403-2 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_90 GBV_ILN_95 GBV_ILN_100 GBV_ILN_105 GBV_ILN_110 GBV_ILN_138 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_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_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_2190 GBV_ILN_2232 GBV_ILN_2336 GBV_ILN_2470 GBV_ILN_2472 GBV_ILN_2507 GBV_ILN_2522 GBV_ILN_4012 GBV_ILN_4035 GBV_ILN_4037 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_4367 GBV_ILN_4393 GBV_ILN_4700 50.00 ASE 35.00 ASE 33.00 ASE AR 2 2020 4 07 03
allfields_unstemmed	10.1007/s42452-020-2403-2 doi (DE-627)SPR039030016 (DE-599)SPRs42452-020-2403-2-e (SPR)s42452-020-2403-2-e DE-627 ger DE-627 rakwb eng 500 ASE 500 ASE 50.00 bkl 35.00 bkl 33.00 bkl Khalid, Muhammad Yasir verfasserin aut Experimental and numerical characterization of tensile property of jute/carbon fabric reinforced epoxy hybrid composites 2020 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier Abstract Jute based green composites are emerging materials due to their certain attractive properties like appropriate strength to weight ratio, high damping ratio, low price and corrosion resistance. Jute/carbon hybrid composite can replace carbon fiber reinforced composites without much loss in tensile strength. These hybrid composites are now being used in various automobile interior and exterior parts. In this study tensile behavior of carbon/jute reinforced epoxy hybrid textile composites, for different volume fractions of carbon and jute fibers, is studied experimentally and numerically. Tensile behavior of composite materials is always required for design and analysis of any structure. It is found that with increase in jute percentage tensile strength of hybrid composite decrease. Numerical results agrees well with experimental results and error increases with increase in jute percentage due to heterogeneous jute properties and waviness of fabrics. Fractographic study reveals that delamination phenomenon exists in between plies and jute fiber shows more pullout than carbon fiber. Scanning electron microscope analysis depicted that matrix fails in form of fragmentation while fibers show pullout during failure. Hybrid composites (dpeaa)DE-He213 CFRP (dpeaa)DE-He213 Laminated textile composites (dpeaa)DE-He213 Simulation (dpeaa)DE-He213 Nasir, Muhammad Ali verfasserin aut Ali, Aakash verfasserin aut Al Rashid, Ans verfasserin aut Khan, Muhammad Riaz verfasserin aut Enthalten in SN applied sciences [Cham] : Springer International Publishing, 2019 2(2020), 4 vom: 07. März (DE-627)103761139X (DE-600)2947292-1 2523-3971 nnns volume:2 year:2020 number:4 day:07 month:03 https://dx.doi.org/10.1007/s42452-020-2403-2 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_90 GBV_ILN_95 GBV_ILN_100 GBV_ILN_105 GBV_ILN_110 GBV_ILN_138 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_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_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_2190 GBV_ILN_2232 GBV_ILN_2336 GBV_ILN_2470 GBV_ILN_2472 GBV_ILN_2507 GBV_ILN_2522 GBV_ILN_4012 GBV_ILN_4035 GBV_ILN_4037 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_4367 GBV_ILN_4393 GBV_ILN_4700 50.00 ASE 35.00 ASE 33.00 ASE AR 2 2020 4 07 03
allfieldsGer	10.1007/s42452-020-2403-2 doi (DE-627)SPR039030016 (DE-599)SPRs42452-020-2403-2-e (SPR)s42452-020-2403-2-e DE-627 ger DE-627 rakwb eng 500 ASE 500 ASE 50.00 bkl 35.00 bkl 33.00 bkl Khalid, Muhammad Yasir verfasserin aut Experimental and numerical characterization of tensile property of jute/carbon fabric reinforced epoxy hybrid composites 2020 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier Abstract Jute based green composites are emerging materials due to their certain attractive properties like appropriate strength to weight ratio, high damping ratio, low price and corrosion resistance. Jute/carbon hybrid composite can replace carbon fiber reinforced composites without much loss in tensile strength. These hybrid composites are now being used in various automobile interior and exterior parts. In this study tensile behavior of carbon/jute reinforced epoxy hybrid textile composites, for different volume fractions of carbon and jute fibers, is studied experimentally and numerically. Tensile behavior of composite materials is always required for design and analysis of any structure. It is found that with increase in jute percentage tensile strength of hybrid composite decrease. Numerical results agrees well with experimental results and error increases with increase in jute percentage due to heterogeneous jute properties and waviness of fabrics. Fractographic study reveals that delamination phenomenon exists in between plies and jute fiber shows more pullout than carbon fiber. Scanning electron microscope analysis depicted that matrix fails in form of fragmentation while fibers show pullout during failure. Hybrid composites (dpeaa)DE-He213 CFRP (dpeaa)DE-He213 Laminated textile composites (dpeaa)DE-He213 Simulation (dpeaa)DE-He213 Nasir, Muhammad Ali verfasserin aut Ali, Aakash verfasserin aut Al Rashid, Ans verfasserin aut Khan, Muhammad Riaz verfasserin aut Enthalten in SN applied sciences [Cham] : Springer International Publishing, 2019 2(2020), 4 vom: 07. März (DE-627)103761139X (DE-600)2947292-1 2523-3971 nnns volume:2 year:2020 number:4 day:07 month:03 https://dx.doi.org/10.1007/s42452-020-2403-2 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_90 GBV_ILN_95 GBV_ILN_100 GBV_ILN_105 GBV_ILN_110 GBV_ILN_138 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_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_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_2190 GBV_ILN_2232 GBV_ILN_2336 GBV_ILN_2470 GBV_ILN_2472 GBV_ILN_2507 GBV_ILN_2522 GBV_ILN_4012 GBV_ILN_4035 GBV_ILN_4037 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_4367 GBV_ILN_4393 GBV_ILN_4700 50.00 ASE 35.00 ASE 33.00 ASE AR 2 2020 4 07 03
allfieldsSound	10.1007/s42452-020-2403-2 doi (DE-627)SPR039030016 (DE-599)SPRs42452-020-2403-2-e (SPR)s42452-020-2403-2-e DE-627 ger DE-627 rakwb eng 500 ASE 500 ASE 50.00 bkl 35.00 bkl 33.00 bkl Khalid, Muhammad Yasir verfasserin aut Experimental and numerical characterization of tensile property of jute/carbon fabric reinforced epoxy hybrid composites 2020 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier Abstract Jute based green composites are emerging materials due to their certain attractive properties like appropriate strength to weight ratio, high damping ratio, low price and corrosion resistance. Jute/carbon hybrid composite can replace carbon fiber reinforced composites without much loss in tensile strength. These hybrid composites are now being used in various automobile interior and exterior parts. In this study tensile behavior of carbon/jute reinforced epoxy hybrid textile composites, for different volume fractions of carbon and jute fibers, is studied experimentally and numerically. Tensile behavior of composite materials is always required for design and analysis of any structure. It is found that with increase in jute percentage tensile strength of hybrid composite decrease. Numerical results agrees well with experimental results and error increases with increase in jute percentage due to heterogeneous jute properties and waviness of fabrics. Fractographic study reveals that delamination phenomenon exists in between plies and jute fiber shows more pullout than carbon fiber. Scanning electron microscope analysis depicted that matrix fails in form of fragmentation while fibers show pullout during failure. Hybrid composites (dpeaa)DE-He213 CFRP (dpeaa)DE-He213 Laminated textile composites (dpeaa)DE-He213 Simulation (dpeaa)DE-He213 Nasir, Muhammad Ali verfasserin aut Ali, Aakash verfasserin aut Al Rashid, Ans verfasserin aut Khan, Muhammad Riaz verfasserin aut Enthalten in SN applied sciences [Cham] : Springer International Publishing, 2019 2(2020), 4 vom: 07. März (DE-627)103761139X (DE-600)2947292-1 2523-3971 nnns volume:2 year:2020 number:4 day:07 month:03 https://dx.doi.org/10.1007/s42452-020-2403-2 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_90 GBV_ILN_95 GBV_ILN_100 GBV_ILN_105 GBV_ILN_110 GBV_ILN_138 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_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_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_2190 GBV_ILN_2232 GBV_ILN_2336 GBV_ILN_2470 GBV_ILN_2472 GBV_ILN_2507 GBV_ILN_2522 GBV_ILN_4012 GBV_ILN_4035 GBV_ILN_4037 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_4367 GBV_ILN_4393 GBV_ILN_4700 50.00 ASE 35.00 ASE 33.00 ASE AR 2 2020 4 07 03
language	English
source	Enthalten in SN applied sciences 2(2020), 4 vom: 07. März volume:2 year:2020 number:4 day:07 month:03
sourceStr	Enthalten in SN applied sciences 2(2020), 4 vom: 07. März volume:2 year:2020 number:4 day:07 month:03
format_phy_str_mv	Article
institution	findex.gbv.de
topic_facet	Hybrid composites CFRP Laminated textile composites Simulation
dewey-raw	500
isfreeaccess_bool	false
container_title	SN applied sciences
authorswithroles_txt_mv	Khalid, Muhammad Yasir @@aut@@ Nasir, Muhammad Ali @@aut@@ Ali, Aakash @@aut@@ Al Rashid, Ans @@aut@@ Khan, Muhammad Riaz @@aut@@
publishDateDaySort_date	2020-03-07T00:00:00Z
hierarchy_top_id	103761139X
dewey-sort	3500
id	SPR039030016
language_de	englisch
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author	Khalid, Muhammad Yasir
spellingShingle	Khalid, Muhammad Yasir ddc 500 bkl 50.00 bkl 35.00 bkl 33.00 misc Hybrid composites misc CFRP misc Laminated textile composites misc Simulation Experimental and numerical characterization of tensile property of jute/carbon fabric reinforced epoxy hybrid composites
authorStr	Khalid, Muhammad Yasir
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topic_title	500 ASE 50.00 bkl 35.00 bkl 33.00 bkl Experimental and numerical characterization of tensile property of jute/carbon fabric reinforced epoxy hybrid composites Hybrid composites (dpeaa)DE-He213 CFRP (dpeaa)DE-He213 Laminated textile composites (dpeaa)DE-He213 Simulation (dpeaa)DE-He213
topic	ddc 500 bkl 50.00 bkl 35.00 bkl 33.00 misc Hybrid composites misc CFRP misc Laminated textile composites misc Simulation
topic_unstemmed	ddc 500 bkl 50.00 bkl 35.00 bkl 33.00 misc Hybrid composites misc CFRP misc Laminated textile composites misc Simulation
topic_browse	ddc 500 bkl 50.00 bkl 35.00 bkl 33.00 misc Hybrid composites misc CFRP misc Laminated textile composites misc Simulation
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title	Experimental and numerical characterization of tensile property of jute/carbon fabric reinforced epoxy hybrid composites
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title_full	Experimental and numerical characterization of tensile property of jute/carbon fabric reinforced epoxy hybrid composites
author_sort	Khalid, Muhammad Yasir
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author_browse	Khalid, Muhammad Yasir Nasir, Muhammad Ali Ali, Aakash Al Rashid, Ans Khan, Muhammad Riaz
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title_sort	experimental and numerical characterization of tensile property of jute/carbon fabric reinforced epoxy hybrid composites
title_auth	Experimental and numerical characterization of tensile property of jute/carbon fabric reinforced epoxy hybrid composites
abstract	Abstract Jute based green composites are emerging materials due to their certain attractive properties like appropriate strength to weight ratio, high damping ratio, low price and corrosion resistance. Jute/carbon hybrid composite can replace carbon fiber reinforced composites without much loss in tensile strength. These hybrid composites are now being used in various automobile interior and exterior parts. In this study tensile behavior of carbon/jute reinforced epoxy hybrid textile composites, for different volume fractions of carbon and jute fibers, is studied experimentally and numerically. Tensile behavior of composite materials is always required for design and analysis of any structure. It is found that with increase in jute percentage tensile strength of hybrid composite decrease. Numerical results agrees well with experimental results and error increases with increase in jute percentage due to heterogeneous jute properties and waviness of fabrics. Fractographic study reveals that delamination phenomenon exists in between plies and jute fiber shows more pullout than carbon fiber. Scanning electron microscope analysis depicted that matrix fails in form of fragmentation while fibers show pullout during failure.
abstractGer	Abstract Jute based green composites are emerging materials due to their certain attractive properties like appropriate strength to weight ratio, high damping ratio, low price and corrosion resistance. Jute/carbon hybrid composite can replace carbon fiber reinforced composites without much loss in tensile strength. These hybrid composites are now being used in various automobile interior and exterior parts. In this study tensile behavior of carbon/jute reinforced epoxy hybrid textile composites, for different volume fractions of carbon and jute fibers, is studied experimentally and numerically. Tensile behavior of composite materials is always required for design and analysis of any structure. It is found that with increase in jute percentage tensile strength of hybrid composite decrease. Numerical results agrees well with experimental results and error increases with increase in jute percentage due to heterogeneous jute properties and waviness of fabrics. Fractographic study reveals that delamination phenomenon exists in between plies and jute fiber shows more pullout than carbon fiber. Scanning electron microscope analysis depicted that matrix fails in form of fragmentation while fibers show pullout during failure.
abstract_unstemmed	Abstract Jute based green composites are emerging materials due to their certain attractive properties like appropriate strength to weight ratio, high damping ratio, low price and corrosion resistance. Jute/carbon hybrid composite can replace carbon fiber reinforced composites without much loss in tensile strength. These hybrid composites are now being used in various automobile interior and exterior parts. In this study tensile behavior of carbon/jute reinforced epoxy hybrid textile composites, for different volume fractions of carbon and jute fibers, is studied experimentally and numerically. Tensile behavior of composite materials is always required for design and analysis of any structure. It is found that with increase in jute percentage tensile strength of hybrid composite decrease. Numerical results agrees well with experimental results and error increases with increase in jute percentage due to heterogeneous jute properties and waviness of fabrics. Fractographic study reveals that delamination phenomenon exists in between plies and jute fiber shows more pullout than carbon fiber. Scanning electron microscope analysis depicted that matrix fails in form of fragmentation while fibers show pullout during failure.
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container_issue	4
title_short	Experimental and numerical characterization of tensile property of jute/carbon fabric reinforced epoxy hybrid composites
url	https://dx.doi.org/10.1007/s42452-020-2403-2
remote_bool	true
author2	Nasir, Muhammad Ali Ali, Aakash Al Rashid, Ans Khan, Muhammad Riaz
author2Str	Nasir, Muhammad Ali Ali, Aakash Al Rashid, Ans Khan, Muhammad Riaz
ppnlink	103761139X
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isOA_txt	false
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doi_str	10.1007/s42452-020-2403-2
up_date	2024-07-03T21:28:43.130Z
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