Crashworthy characteristics of axial quasi-statically compressed Bombyx mori composite cylindrical tubes: Experimental

Abstract The study investigated the energy absorption response and load carrying capability of Bombyx mori (B. mori) natural silk fibre/epoxy composite cylindrical tubes subjected to an axial quasi-static crushing test. The reinforced cylindrical composite tubes were prepared using hand lay-up techn...
Ausführliche Beschreibung

Gespeichert in:

Autor*in:	Ude, A. U. [verfasserIn] Eshkoor, R. A. Azhari, C. H.

Format:	E-Artikel
Sprache:	Englisch

Erschienen:	2017

Schlagwörter:	woven fibres Laminated composite Crashworthiness

Anmerkung:	© The Korean Fiber Society and Springer Science+Business Media B.V. 2017

Übergeordnetes Werk:	Enthalten in: Fibers and polymers - Seoul : The Korean Fiber Society, 2000, 18(2017), 8 vom: Aug., Seite 1594-1601
Übergeordnetes Werk:	volume:18 ; year:2017 ; number:8 ; month:08 ; pages:1594-1601

Links:	Volltext

DOI / URN:	10.1007/s12221-017-1235-1

Katalog-ID:	SPR025440039

Internformat


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245	1	0	\|a Crashworthy characteristics of axial quasi-statically compressed Bombyx mori composite cylindrical tubes: Experimental
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520			\|a Abstract The study investigated the energy absorption response and load carrying capability of Bombyx mori (B. mori) natural silk fibre/epoxy composite cylindrical tubes subjected to an axial quasi-static crushing test. The reinforced cylindrical composite tubes were prepared using hand lay-up technique. Varied numbers of B. mori layers, 12, 24 and 30 were used to fabricate the tubes; their corresponding diameters were 33.3, 62.3 and 80.6 respectively. The crashworthiness of the cylindrical tube was analyzed by measuring the specific energy absorption, peak load and total energy absorption as a function of tube diameter/number of layers under a quasi-static axial compression load. Failure mechanisms of the tubes were analyzed using scan electron microscopy (SEM) and high resolution photographs obtained during test. Generally, the result showed increase in crashworthiness behaviour as the numbers of B. mori layers increased. The 12 layer tube (33.3 mm diameter) showed a progressive crushing failure starting from the upper half; the 24 layer tube (62.3 mm diameter) depict a mid-length crack failure, while the 30 layer tube (80.6 mm diameter) showed a progressive crushing failure from the lower side of the tube. The SEM micrographs of suggest that failure mechanism includes: matrix crack, fiber delamination, fiber pull out, tear and fibre breakage.
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700	1		\|a Azhari, C. H. \|4 aut
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912			\|a GBV_ILN_285
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912			\|a GBV_ILN_636
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912			\|a GBV_ILN_2008
912			\|a GBV_ILN_2009
912			\|a GBV_ILN_2010
912			\|a GBV_ILN_2011
912			\|a GBV_ILN_2014
912			\|a GBV_ILN_2015
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author_variant	a u u au auu r a e ra rae c h a ch cha
matchkey_str	article:18750052:2017----::rswrhcaatrsisfxaqaittclyopesdobxoiopstc
hierarchy_sort_str	2017
publishDate	2017
allfields	10.1007/s12221-017-1235-1 doi (DE-627)SPR025440039 (SPR)s12221-017-1235-1-e DE-627 ger DE-627 rakwb eng Ude, A. U. verfasserin aut Crashworthy characteristics of axial quasi-statically compressed Bombyx mori composite cylindrical tubes: Experimental 2017 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier © The Korean Fiber Society and Springer Science+Business Media B.V. 2017 Abstract The study investigated the energy absorption response and load carrying capability of Bombyx mori (B. mori) natural silk fibre/epoxy composite cylindrical tubes subjected to an axial quasi-static crushing test. The reinforced cylindrical composite tubes were prepared using hand lay-up technique. Varied numbers of B. mori layers, 12, 24 and 30 were used to fabricate the tubes; their corresponding diameters were 33.3, 62.3 and 80.6 respectively. The crashworthiness of the cylindrical tube was analyzed by measuring the specific energy absorption, peak load and total energy absorption as a function of tube diameter/number of layers under a quasi-static axial compression load. Failure mechanisms of the tubes were analyzed using scan electron microscopy (SEM) and high resolution photographs obtained during test. Generally, the result showed increase in crashworthiness behaviour as the numbers of B. mori layers increased. The 12 layer tube (33.3 mm diameter) showed a progressive crushing failure starting from the upper half; the 24 layer tube (62.3 mm diameter) depict a mid-length crack failure, while the 30 layer tube (80.6 mm diameter) showed a progressive crushing failure from the lower side of the tube. The SEM micrographs of suggest that failure mechanism includes: matrix crack, fiber delamination, fiber pull out, tear and fibre breakage. woven fibres (dpeaa)DE-He213 Laminated composite (dpeaa)DE-He213 Crashworthiness (dpeaa)DE-He213 Eshkoor, R. A. aut Azhari, C. H. aut Enthalten in Fibers and polymers Seoul : The Korean Fiber Society, 2000 18(2017), 8 vom: Aug., Seite 1594-1601 (DE-627)565516485 (DE-600)2424081-3 1875-0052 nnns volume:18 year:2017 number:8 month:08 pages:1594-1601 https://dx.doi.org/10.1007/s12221-017-1235-1 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_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 18 2017 8 08 1594-1601
spelling	10.1007/s12221-017-1235-1 doi (DE-627)SPR025440039 (SPR)s12221-017-1235-1-e DE-627 ger DE-627 rakwb eng Ude, A. U. verfasserin aut Crashworthy characteristics of axial quasi-statically compressed Bombyx mori composite cylindrical tubes: Experimental 2017 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier © The Korean Fiber Society and Springer Science+Business Media B.V. 2017 Abstract The study investigated the energy absorption response and load carrying capability of Bombyx mori (B. mori) natural silk fibre/epoxy composite cylindrical tubes subjected to an axial quasi-static crushing test. The reinforced cylindrical composite tubes were prepared using hand lay-up technique. Varied numbers of B. mori layers, 12, 24 and 30 were used to fabricate the tubes; their corresponding diameters were 33.3, 62.3 and 80.6 respectively. The crashworthiness of the cylindrical tube was analyzed by measuring the specific energy absorption, peak load and total energy absorption as a function of tube diameter/number of layers under a quasi-static axial compression load. Failure mechanisms of the tubes were analyzed using scan electron microscopy (SEM) and high resolution photographs obtained during test. Generally, the result showed increase in crashworthiness behaviour as the numbers of B. mori layers increased. The 12 layer tube (33.3 mm diameter) showed a progressive crushing failure starting from the upper half; the 24 layer tube (62.3 mm diameter) depict a mid-length crack failure, while the 30 layer tube (80.6 mm diameter) showed a progressive crushing failure from the lower side of the tube. The SEM micrographs of suggest that failure mechanism includes: matrix crack, fiber delamination, fiber pull out, tear and fibre breakage. woven fibres (dpeaa)DE-He213 Laminated composite (dpeaa)DE-He213 Crashworthiness (dpeaa)DE-He213 Eshkoor, R. A. aut Azhari, C. H. aut Enthalten in Fibers and polymers Seoul : The Korean Fiber Society, 2000 18(2017), 8 vom: Aug., Seite 1594-1601 (DE-627)565516485 (DE-600)2424081-3 1875-0052 nnns volume:18 year:2017 number:8 month:08 pages:1594-1601 https://dx.doi.org/10.1007/s12221-017-1235-1 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_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 18 2017 8 08 1594-1601
allfields_unstemmed	10.1007/s12221-017-1235-1 doi (DE-627)SPR025440039 (SPR)s12221-017-1235-1-e DE-627 ger DE-627 rakwb eng Ude, A. U. verfasserin aut Crashworthy characteristics of axial quasi-statically compressed Bombyx mori composite cylindrical tubes: Experimental 2017 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier © The Korean Fiber Society and Springer Science+Business Media B.V. 2017 Abstract The study investigated the energy absorption response and load carrying capability of Bombyx mori (B. mori) natural silk fibre/epoxy composite cylindrical tubes subjected to an axial quasi-static crushing test. The reinforced cylindrical composite tubes were prepared using hand lay-up technique. Varied numbers of B. mori layers, 12, 24 and 30 were used to fabricate the tubes; their corresponding diameters were 33.3, 62.3 and 80.6 respectively. The crashworthiness of the cylindrical tube was analyzed by measuring the specific energy absorption, peak load and total energy absorption as a function of tube diameter/number of layers under a quasi-static axial compression load. Failure mechanisms of the tubes were analyzed using scan electron microscopy (SEM) and high resolution photographs obtained during test. Generally, the result showed increase in crashworthiness behaviour as the numbers of B. mori layers increased. The 12 layer tube (33.3 mm diameter) showed a progressive crushing failure starting from the upper half; the 24 layer tube (62.3 mm diameter) depict a mid-length crack failure, while the 30 layer tube (80.6 mm diameter) showed a progressive crushing failure from the lower side of the tube. The SEM micrographs of suggest that failure mechanism includes: matrix crack, fiber delamination, fiber pull out, tear and fibre breakage. woven fibres (dpeaa)DE-He213 Laminated composite (dpeaa)DE-He213 Crashworthiness (dpeaa)DE-He213 Eshkoor, R. A. aut Azhari, C. H. aut Enthalten in Fibers and polymers Seoul : The Korean Fiber Society, 2000 18(2017), 8 vom: Aug., Seite 1594-1601 (DE-627)565516485 (DE-600)2424081-3 1875-0052 nnns volume:18 year:2017 number:8 month:08 pages:1594-1601 https://dx.doi.org/10.1007/s12221-017-1235-1 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_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 18 2017 8 08 1594-1601
allfieldsGer	10.1007/s12221-017-1235-1 doi (DE-627)SPR025440039 (SPR)s12221-017-1235-1-e DE-627 ger DE-627 rakwb eng Ude, A. U. verfasserin aut Crashworthy characteristics of axial quasi-statically compressed Bombyx mori composite cylindrical tubes: Experimental 2017 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier © The Korean Fiber Society and Springer Science+Business Media B.V. 2017 Abstract The study investigated the energy absorption response and load carrying capability of Bombyx mori (B. mori) natural silk fibre/epoxy composite cylindrical tubes subjected to an axial quasi-static crushing test. The reinforced cylindrical composite tubes were prepared using hand lay-up technique. Varied numbers of B. mori layers, 12, 24 and 30 were used to fabricate the tubes; their corresponding diameters were 33.3, 62.3 and 80.6 respectively. The crashworthiness of the cylindrical tube was analyzed by measuring the specific energy absorption, peak load and total energy absorption as a function of tube diameter/number of layers under a quasi-static axial compression load. Failure mechanisms of the tubes were analyzed using scan electron microscopy (SEM) and high resolution photographs obtained during test. Generally, the result showed increase in crashworthiness behaviour as the numbers of B. mori layers increased. The 12 layer tube (33.3 mm diameter) showed a progressive crushing failure starting from the upper half; the 24 layer tube (62.3 mm diameter) depict a mid-length crack failure, while the 30 layer tube (80.6 mm diameter) showed a progressive crushing failure from the lower side of the tube. The SEM micrographs of suggest that failure mechanism includes: matrix crack, fiber delamination, fiber pull out, tear and fibre breakage. woven fibres (dpeaa)DE-He213 Laminated composite (dpeaa)DE-He213 Crashworthiness (dpeaa)DE-He213 Eshkoor, R. A. aut Azhari, C. H. aut Enthalten in Fibers and polymers Seoul : The Korean Fiber Society, 2000 18(2017), 8 vom: Aug., Seite 1594-1601 (DE-627)565516485 (DE-600)2424081-3 1875-0052 nnns volume:18 year:2017 number:8 month:08 pages:1594-1601 https://dx.doi.org/10.1007/s12221-017-1235-1 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_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 18 2017 8 08 1594-1601
allfieldsSound	10.1007/s12221-017-1235-1 doi (DE-627)SPR025440039 (SPR)s12221-017-1235-1-e DE-627 ger DE-627 rakwb eng Ude, A. U. verfasserin aut Crashworthy characteristics of axial quasi-statically compressed Bombyx mori composite cylindrical tubes: Experimental 2017 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier © The Korean Fiber Society and Springer Science+Business Media B.V. 2017 Abstract The study investigated the energy absorption response and load carrying capability of Bombyx mori (B. mori) natural silk fibre/epoxy composite cylindrical tubes subjected to an axial quasi-static crushing test. The reinforced cylindrical composite tubes were prepared using hand lay-up technique. Varied numbers of B. mori layers, 12, 24 and 30 were used to fabricate the tubes; their corresponding diameters were 33.3, 62.3 and 80.6 respectively. The crashworthiness of the cylindrical tube was analyzed by measuring the specific energy absorption, peak load and total energy absorption as a function of tube diameter/number of layers under a quasi-static axial compression load. Failure mechanisms of the tubes were analyzed using scan electron microscopy (SEM) and high resolution photographs obtained during test. Generally, the result showed increase in crashworthiness behaviour as the numbers of B. mori layers increased. The 12 layer tube (33.3 mm diameter) showed a progressive crushing failure starting from the upper half; the 24 layer tube (62.3 mm diameter) depict a mid-length crack failure, while the 30 layer tube (80.6 mm diameter) showed a progressive crushing failure from the lower side of the tube. The SEM micrographs of suggest that failure mechanism includes: matrix crack, fiber delamination, fiber pull out, tear and fibre breakage. woven fibres (dpeaa)DE-He213 Laminated composite (dpeaa)DE-He213 Crashworthiness (dpeaa)DE-He213 Eshkoor, R. A. aut Azhari, C. H. aut Enthalten in Fibers and polymers Seoul : The Korean Fiber Society, 2000 18(2017), 8 vom: Aug., Seite 1594-1601 (DE-627)565516485 (DE-600)2424081-3 1875-0052 nnns volume:18 year:2017 number:8 month:08 pages:1594-1601 https://dx.doi.org/10.1007/s12221-017-1235-1 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_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 18 2017 8 08 1594-1601
language	English
source	Enthalten in Fibers and polymers 18(2017), 8 vom: Aug., Seite 1594-1601 volume:18 year:2017 number:8 month:08 pages:1594-1601
sourceStr	Enthalten in Fibers and polymers 18(2017), 8 vom: Aug., Seite 1594-1601 volume:18 year:2017 number:8 month:08 pages:1594-1601
format_phy_str_mv	Article
institution	findex.gbv.de
topic_facet	woven fibres Laminated composite Crashworthiness
isfreeaccess_bool	false
container_title	Fibers and polymers
authorswithroles_txt_mv	Ude, A. U. @@aut@@ Eshkoor, R. A. @@aut@@ Azhari, C. H. @@aut@@
publishDateDaySort_date	2017-08-01T00:00:00Z
hierarchy_top_id	565516485
id	SPR025440039
language_de	englisch
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U.</subfield><subfield code="e">verfasserin</subfield><subfield code="4">aut</subfield></datafield><datafield tag="245" ind1="1" ind2="0"><subfield code="a">Crashworthy characteristics of axial quasi-statically compressed Bombyx mori composite cylindrical tubes: Experimental</subfield></datafield><datafield tag="264" ind1=" " ind2="1"><subfield code="c">2017</subfield></datafield><datafield tag="336" ind1=" " ind2=" "><subfield code="a">Text</subfield><subfield code="b">txt</subfield><subfield code="2">rdacontent</subfield></datafield><datafield tag="337" ind1=" " ind2=" "><subfield code="a">Computermedien</subfield><subfield code="b">c</subfield><subfield code="2">rdamedia</subfield></datafield><datafield tag="338" ind1=" " ind2=" "><subfield code="a">Online-Ressource</subfield><subfield code="b">cr</subfield><subfield code="2">rdacarrier</subfield></datafield><datafield tag="500" ind1=" " ind2=" "><subfield code="a">© The Korean Fiber Society and Springer Science+Business Media B.V. 2017</subfield></datafield><datafield tag="520" ind1=" " ind2=" "><subfield code="a">Abstract The study investigated the energy absorption response and load carrying capability of Bombyx mori (B. mori) natural silk fibre/epoxy composite cylindrical tubes subjected to an axial quasi-static crushing test. The reinforced cylindrical composite tubes were prepared using hand lay-up technique. Varied numbers of B. mori layers, 12, 24 and 30 were used to fabricate the tubes; their corresponding diameters were 33.3, 62.3 and 80.6 respectively. The crashworthiness of the cylindrical tube was analyzed by measuring the specific energy absorption, peak load and total energy absorption as a function of tube diameter/number of layers under a quasi-static axial compression load. Failure mechanisms of the tubes were analyzed using scan electron microscopy (SEM) and high resolution photographs obtained during test. Generally, the result showed increase in crashworthiness behaviour as the numbers of B. mori layers increased. 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author	Ude, A. U.
spellingShingle	Ude, A. U. misc woven fibres misc Laminated composite misc Crashworthiness Crashworthy characteristics of axial quasi-statically compressed Bombyx mori composite cylindrical tubes: Experimental
authorStr	Ude, A. U.
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topic_title	Crashworthy characteristics of axial quasi-statically compressed Bombyx mori composite cylindrical tubes: Experimental woven fibres (dpeaa)DE-He213 Laminated composite (dpeaa)DE-He213 Crashworthiness (dpeaa)DE-He213
topic	misc woven fibres misc Laminated composite misc Crashworthiness
topic_unstemmed	misc woven fibres misc Laminated composite misc Crashworthiness
topic_browse	misc woven fibres misc Laminated composite misc Crashworthiness
format_facet	Elektronische Aufsätze Aufsätze Elektronische Ressource
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title	Crashworthy characteristics of axial quasi-statically compressed Bombyx mori composite cylindrical tubes: Experimental
ctrlnum	(DE-627)SPR025440039 (SPR)s12221-017-1235-1-e
title_full	Crashworthy characteristics of axial quasi-statically compressed Bombyx mori composite cylindrical tubes: Experimental
author_sort	Ude, A. U.
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author_browse	Ude, A. U. Eshkoor, R. A. Azhari, C. H.
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author-letter	Ude, A. U.
doi_str_mv	10.1007/s12221-017-1235-1
title_sort	crashworthy characteristics of axial quasi-statically compressed bombyx mori composite cylindrical tubes: experimental
title_auth	Crashworthy characteristics of axial quasi-statically compressed Bombyx mori composite cylindrical tubes: Experimental
abstract	Abstract The study investigated the energy absorption response and load carrying capability of Bombyx mori (B. mori) natural silk fibre/epoxy composite cylindrical tubes subjected to an axial quasi-static crushing test. The reinforced cylindrical composite tubes were prepared using hand lay-up technique. Varied numbers of B. mori layers, 12, 24 and 30 were used to fabricate the tubes; their corresponding diameters were 33.3, 62.3 and 80.6 respectively. The crashworthiness of the cylindrical tube was analyzed by measuring the specific energy absorption, peak load and total energy absorption as a function of tube diameter/number of layers under a quasi-static axial compression load. Failure mechanisms of the tubes were analyzed using scan electron microscopy (SEM) and high resolution photographs obtained during test. Generally, the result showed increase in crashworthiness behaviour as the numbers of B. mori layers increased. The 12 layer tube (33.3 mm diameter) showed a progressive crushing failure starting from the upper half; the 24 layer tube (62.3 mm diameter) depict a mid-length crack failure, while the 30 layer tube (80.6 mm diameter) showed a progressive crushing failure from the lower side of the tube. The SEM micrographs of suggest that failure mechanism includes: matrix crack, fiber delamination, fiber pull out, tear and fibre breakage. © The Korean Fiber Society and Springer Science+Business Media B.V. 2017
abstractGer	Abstract The study investigated the energy absorption response and load carrying capability of Bombyx mori (B. mori) natural silk fibre/epoxy composite cylindrical tubes subjected to an axial quasi-static crushing test. The reinforced cylindrical composite tubes were prepared using hand lay-up technique. Varied numbers of B. mori layers, 12, 24 and 30 were used to fabricate the tubes; their corresponding diameters were 33.3, 62.3 and 80.6 respectively. The crashworthiness of the cylindrical tube was analyzed by measuring the specific energy absorption, peak load and total energy absorption as a function of tube diameter/number of layers under a quasi-static axial compression load. Failure mechanisms of the tubes were analyzed using scan electron microscopy (SEM) and high resolution photographs obtained during test. Generally, the result showed increase in crashworthiness behaviour as the numbers of B. mori layers increased. The 12 layer tube (33.3 mm diameter) showed a progressive crushing failure starting from the upper half; the 24 layer tube (62.3 mm diameter) depict a mid-length crack failure, while the 30 layer tube (80.6 mm diameter) showed a progressive crushing failure from the lower side of the tube. The SEM micrographs of suggest that failure mechanism includes: matrix crack, fiber delamination, fiber pull out, tear and fibre breakage. © The Korean Fiber Society and Springer Science+Business Media B.V. 2017
abstract_unstemmed	Abstract The study investigated the energy absorption response and load carrying capability of Bombyx mori (B. mori) natural silk fibre/epoxy composite cylindrical tubes subjected to an axial quasi-static crushing test. The reinforced cylindrical composite tubes were prepared using hand lay-up technique. Varied numbers of B. mori layers, 12, 24 and 30 were used to fabricate the tubes; their corresponding diameters were 33.3, 62.3 and 80.6 respectively. The crashworthiness of the cylindrical tube was analyzed by measuring the specific energy absorption, peak load and total energy absorption as a function of tube diameter/number of layers under a quasi-static axial compression load. Failure mechanisms of the tubes were analyzed using scan electron microscopy (SEM) and high resolution photographs obtained during test. Generally, the result showed increase in crashworthiness behaviour as the numbers of B. mori layers increased. The 12 layer tube (33.3 mm diameter) showed a progressive crushing failure starting from the upper half; the 24 layer tube (62.3 mm diameter) depict a mid-length crack failure, while the 30 layer tube (80.6 mm diameter) showed a progressive crushing failure from the lower side of the tube. The SEM micrographs of suggest that failure mechanism includes: matrix crack, fiber delamination, fiber pull out, tear and fibre breakage. © The Korean Fiber Society and Springer Science+Business Media B.V. 2017
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container_issue	8
title_short	Crashworthy characteristics of axial quasi-statically compressed Bombyx mori composite cylindrical tubes: Experimental
url	https://dx.doi.org/10.1007/s12221-017-1235-1
remote_bool	true
author2	Eshkoor, R. A. Azhari, C. H.
author2Str	Eshkoor, R. A. Azhari, C. H.
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doi_str	10.1007/s12221-017-1235-1
up_date	2024-07-03T16:00:32.111Z
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Crashworthy characteristics of axial quasi-statically compressed Bombyx mori composite cylindrical tubes: Experimental

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