Finite element modelling of creep deformation in fibre-reinforced ceramic composites

Abstract The tensile creep and creep-recovery behaviour of a unidirectional SiC fibre-$ Si_{3} $$ N_{4} $ matrix composite was analysed using finite element techniques. The analysis, based on the elastic and creep properties of each constituent, considered the influence of fibre-matrix bonding and p...
Ausführliche Beschreibung

Gespeichert in:

Autor*in:	Park, Y. H. [verfasserIn] Holmes, J. W.

Format:	Artikel
Sprache:	Englisch

Erschienen:	1992

Schlagwörter:	Residual Stress Creep Rate Creep Strain Creep Deformation Creep Property

Anmerkung:	© Chapman & Hall 1992

Übergeordnetes Werk:	Enthalten in: Journal of materials science - Kluwer Academic Publishers-Plenum Publishers, 1966, 27(1992), 23 vom: 01. Jan., Seite 6341-6351
Übergeordnetes Werk:	volume:27 ; year:1992 ; number:23 ; day:01 ; month:01 ; pages:6341-6351

Links:	Volltext

DOI / URN:	10.1007/BF00576283

Katalog-ID:	OLC2046194926

Internformat


LEADER	01000caa a22002652 4500
001	OLC2046194926
003	DE-627
005	20230503122250.0
007	tu
008	200820s1992 xx \|\|\|\|\| 00\| \|\|eng c
024	7		\|a 10.1007/BF00576283 \|2 doi
035			\|a (DE-627)OLC2046194926
035			\|a (DE-He213)BF00576283-p
040			\|a DE-627 \|b ger \|c DE-627 \|e rakwb
041			\|a eng
082	0	4	\|a 670 \|q VZ
100	1		\|a Park, Y. H. \|e verfasserin \|4 aut
245	1	0	\|a Finite element modelling of creep deformation in fibre-reinforced ceramic composites
264		1	\|c 1992
336			\|a Text \|b txt \|2 rdacontent
337			\|a ohne Hilfsmittel zu benutzen \|b n \|2 rdamedia
338			\|a Band \|b nc \|2 rdacarrier
500			\|a © Chapman & Hall 1992
520			\|a Abstract The tensile creep and creep-recovery behaviour of a unidirectional SiC fibre-$ Si_{3} $$ N_{4} $ matrix composite was analysed using finite element techniques. The analysis, based on the elastic and creep properties of each constituent, considered the influence of fibre-matrix bonding and processing-related residual stresses on creep and creep-recovery behaviour. Both two- and three-dimensional finite element models were used. Although both analyses predicted similar overall creep rates, three-dimensional stress analysis was required to obtain detailed information about the stress state in the vicinity of the fibre-matrix interface. The results of the analysis indicate that the tensile radial stress, which develops in the vicinity of the fibre-matrix interface after processing, rapidly decreases during the initial stages of creep. Both the predicted and experimental results for the composite show that 50% of the total creep strain which accumulated after 200 h at a stress of 200 MPa and temperature of 1200°C is recovered within 25 h of unloading.
650		4	\|a Residual Stress
650		4	\|a Creep Rate
650		4	\|a Creep Strain
650		4	\|a Creep Deformation
650		4	\|a Creep Property
700	1		\|a Holmes, J. W. \|4 aut
773	0	8	\|i Enthalten in \|t Journal of materials science \|d Kluwer Academic Publishers-Plenum Publishers, 1966 \|g 27(1992), 23 vom: 01. Jan., Seite 6341-6351 \|w (DE-627)129546372 \|w (DE-600)218324-9 \|w (DE-576)014996774 \|x 0022-2461 \|7 nnns
773	1	8	\|g volume:27 \|g year:1992 \|g number:23 \|g day:01 \|g month:01 \|g pages:6341-6351
856	4	1	\|u https://doi.org/10.1007/BF00576283 \|z lizenzpflichtig \|3 Volltext
912			\|a GBV_USEFLAG_A
912			\|a SYSFLAG_A
912			\|a GBV_OLC
912			\|a SSG-OLC-TEC
912			\|a GBV_ILN_11
912			\|a GBV_ILN_20
912			\|a GBV_ILN_23
912			\|a GBV_ILN_30
912			\|a GBV_ILN_32
912			\|a GBV_ILN_40
912			\|a GBV_ILN_62
912			\|a GBV_ILN_65
912			\|a GBV_ILN_70
912			\|a GBV_ILN_2004
912			\|a GBV_ILN_2006
912			\|a GBV_ILN_2015
912			\|a GBV_ILN_2020
912			\|a GBV_ILN_2021
912			\|a GBV_ILN_4082
912			\|a GBV_ILN_4305
912			\|a GBV_ILN_4306
912			\|a GBV_ILN_4316
912			\|a GBV_ILN_4319
912			\|a GBV_ILN_4323
912			\|a GBV_ILN_4700
951			\|a AR
952			\|d 27 \|j 1992 \|e 23 \|b 01 \|c 01 \|h 6341-6351

Indexfelder

author_variant	y h p yh yhp j w h jw jwh
matchkey_str	article:00222461:1992----::iielmnmdligfredfrainnirrifr
hierarchy_sort_str	1992
publishDate	1992
allfields	10.1007/BF00576283 doi (DE-627)OLC2046194926 (DE-He213)BF00576283-p DE-627 ger DE-627 rakwb eng 670 VZ Park, Y. H. verfasserin aut Finite element modelling of creep deformation in fibre-reinforced ceramic composites 1992 Text txt rdacontent ohne Hilfsmittel zu benutzen n rdamedia Band nc rdacarrier © Chapman & Hall 1992 Abstract The tensile creep and creep-recovery behaviour of a unidirectional SiC fibre-$ Si_{3} $$ N_{4} $ matrix composite was analysed using finite element techniques. The analysis, based on the elastic and creep properties of each constituent, considered the influence of fibre-matrix bonding and processing-related residual stresses on creep and creep-recovery behaviour. Both two- and three-dimensional finite element models were used. Although both analyses predicted similar overall creep rates, three-dimensional stress analysis was required to obtain detailed information about the stress state in the vicinity of the fibre-matrix interface. The results of the analysis indicate that the tensile radial stress, which develops in the vicinity of the fibre-matrix interface after processing, rapidly decreases during the initial stages of creep. Both the predicted and experimental results for the composite show that 50% of the total creep strain which accumulated after 200 h at a stress of 200 MPa and temperature of 1200°C is recovered within 25 h of unloading. Residual Stress Creep Rate Creep Strain Creep Deformation Creep Property Holmes, J. W. aut Enthalten in Journal of materials science Kluwer Academic Publishers-Plenum Publishers, 1966 27(1992), 23 vom: 01. Jan., Seite 6341-6351 (DE-627)129546372 (DE-600)218324-9 (DE-576)014996774 0022-2461 nnns volume:27 year:1992 number:23 day:01 month:01 pages:6341-6351 https://doi.org/10.1007/BF00576283 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_OLC SSG-OLC-TEC GBV_ILN_11 GBV_ILN_20 GBV_ILN_23 GBV_ILN_30 GBV_ILN_32 GBV_ILN_40 GBV_ILN_62 GBV_ILN_65 GBV_ILN_70 GBV_ILN_2004 GBV_ILN_2006 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_4082 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4316 GBV_ILN_4319 GBV_ILN_4323 GBV_ILN_4700 AR 27 1992 23 01 01 6341-6351
spelling	10.1007/BF00576283 doi (DE-627)OLC2046194926 (DE-He213)BF00576283-p DE-627 ger DE-627 rakwb eng 670 VZ Park, Y. H. verfasserin aut Finite element modelling of creep deformation in fibre-reinforced ceramic composites 1992 Text txt rdacontent ohne Hilfsmittel zu benutzen n rdamedia Band nc rdacarrier © Chapman & Hall 1992 Abstract The tensile creep and creep-recovery behaviour of a unidirectional SiC fibre-$ Si_{3} $$ N_{4} $ matrix composite was analysed using finite element techniques. The analysis, based on the elastic and creep properties of each constituent, considered the influence of fibre-matrix bonding and processing-related residual stresses on creep and creep-recovery behaviour. Both two- and three-dimensional finite element models were used. Although both analyses predicted similar overall creep rates, three-dimensional stress analysis was required to obtain detailed information about the stress state in the vicinity of the fibre-matrix interface. The results of the analysis indicate that the tensile radial stress, which develops in the vicinity of the fibre-matrix interface after processing, rapidly decreases during the initial stages of creep. Both the predicted and experimental results for the composite show that 50% of the total creep strain which accumulated after 200 h at a stress of 200 MPa and temperature of 1200°C is recovered within 25 h of unloading. Residual Stress Creep Rate Creep Strain Creep Deformation Creep Property Holmes, J. W. aut Enthalten in Journal of materials science Kluwer Academic Publishers-Plenum Publishers, 1966 27(1992), 23 vom: 01. Jan., Seite 6341-6351 (DE-627)129546372 (DE-600)218324-9 (DE-576)014996774 0022-2461 nnns volume:27 year:1992 number:23 day:01 month:01 pages:6341-6351 https://doi.org/10.1007/BF00576283 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_OLC SSG-OLC-TEC GBV_ILN_11 GBV_ILN_20 GBV_ILN_23 GBV_ILN_30 GBV_ILN_32 GBV_ILN_40 GBV_ILN_62 GBV_ILN_65 GBV_ILN_70 GBV_ILN_2004 GBV_ILN_2006 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_4082 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4316 GBV_ILN_4319 GBV_ILN_4323 GBV_ILN_4700 AR 27 1992 23 01 01 6341-6351
allfields_unstemmed	10.1007/BF00576283 doi (DE-627)OLC2046194926 (DE-He213)BF00576283-p DE-627 ger DE-627 rakwb eng 670 VZ Park, Y. H. verfasserin aut Finite element modelling of creep deformation in fibre-reinforced ceramic composites 1992 Text txt rdacontent ohne Hilfsmittel zu benutzen n rdamedia Band nc rdacarrier © Chapman & Hall 1992 Abstract The tensile creep and creep-recovery behaviour of a unidirectional SiC fibre-$ Si_{3} $$ N_{4} $ matrix composite was analysed using finite element techniques. The analysis, based on the elastic and creep properties of each constituent, considered the influence of fibre-matrix bonding and processing-related residual stresses on creep and creep-recovery behaviour. Both two- and three-dimensional finite element models were used. Although both analyses predicted similar overall creep rates, three-dimensional stress analysis was required to obtain detailed information about the stress state in the vicinity of the fibre-matrix interface. The results of the analysis indicate that the tensile radial stress, which develops in the vicinity of the fibre-matrix interface after processing, rapidly decreases during the initial stages of creep. Both the predicted and experimental results for the composite show that 50% of the total creep strain which accumulated after 200 h at a stress of 200 MPa and temperature of 1200°C is recovered within 25 h of unloading. Residual Stress Creep Rate Creep Strain Creep Deformation Creep Property Holmes, J. W. aut Enthalten in Journal of materials science Kluwer Academic Publishers-Plenum Publishers, 1966 27(1992), 23 vom: 01. Jan., Seite 6341-6351 (DE-627)129546372 (DE-600)218324-9 (DE-576)014996774 0022-2461 nnns volume:27 year:1992 number:23 day:01 month:01 pages:6341-6351 https://doi.org/10.1007/BF00576283 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_OLC SSG-OLC-TEC GBV_ILN_11 GBV_ILN_20 GBV_ILN_23 GBV_ILN_30 GBV_ILN_32 GBV_ILN_40 GBV_ILN_62 GBV_ILN_65 GBV_ILN_70 GBV_ILN_2004 GBV_ILN_2006 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_4082 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4316 GBV_ILN_4319 GBV_ILN_4323 GBV_ILN_4700 AR 27 1992 23 01 01 6341-6351
allfieldsGer	10.1007/BF00576283 doi (DE-627)OLC2046194926 (DE-He213)BF00576283-p DE-627 ger DE-627 rakwb eng 670 VZ Park, Y. H. verfasserin aut Finite element modelling of creep deformation in fibre-reinforced ceramic composites 1992 Text txt rdacontent ohne Hilfsmittel zu benutzen n rdamedia Band nc rdacarrier © Chapman & Hall 1992 Abstract The tensile creep and creep-recovery behaviour of a unidirectional SiC fibre-$ Si_{3} $$ N_{4} $ matrix composite was analysed using finite element techniques. The analysis, based on the elastic and creep properties of each constituent, considered the influence of fibre-matrix bonding and processing-related residual stresses on creep and creep-recovery behaviour. Both two- and three-dimensional finite element models were used. Although both analyses predicted similar overall creep rates, three-dimensional stress analysis was required to obtain detailed information about the stress state in the vicinity of the fibre-matrix interface. The results of the analysis indicate that the tensile radial stress, which develops in the vicinity of the fibre-matrix interface after processing, rapidly decreases during the initial stages of creep. Both the predicted and experimental results for the composite show that 50% of the total creep strain which accumulated after 200 h at a stress of 200 MPa and temperature of 1200°C is recovered within 25 h of unloading. Residual Stress Creep Rate Creep Strain Creep Deformation Creep Property Holmes, J. W. aut Enthalten in Journal of materials science Kluwer Academic Publishers-Plenum Publishers, 1966 27(1992), 23 vom: 01. Jan., Seite 6341-6351 (DE-627)129546372 (DE-600)218324-9 (DE-576)014996774 0022-2461 nnns volume:27 year:1992 number:23 day:01 month:01 pages:6341-6351 https://doi.org/10.1007/BF00576283 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_OLC SSG-OLC-TEC GBV_ILN_11 GBV_ILN_20 GBV_ILN_23 GBV_ILN_30 GBV_ILN_32 GBV_ILN_40 GBV_ILN_62 GBV_ILN_65 GBV_ILN_70 GBV_ILN_2004 GBV_ILN_2006 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_4082 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4316 GBV_ILN_4319 GBV_ILN_4323 GBV_ILN_4700 AR 27 1992 23 01 01 6341-6351
allfieldsSound	10.1007/BF00576283 doi (DE-627)OLC2046194926 (DE-He213)BF00576283-p DE-627 ger DE-627 rakwb eng 670 VZ Park, Y. H. verfasserin aut Finite element modelling of creep deformation in fibre-reinforced ceramic composites 1992 Text txt rdacontent ohne Hilfsmittel zu benutzen n rdamedia Band nc rdacarrier © Chapman & Hall 1992 Abstract The tensile creep and creep-recovery behaviour of a unidirectional SiC fibre-$ Si_{3} $$ N_{4} $ matrix composite was analysed using finite element techniques. The analysis, based on the elastic and creep properties of each constituent, considered the influence of fibre-matrix bonding and processing-related residual stresses on creep and creep-recovery behaviour. Both two- and three-dimensional finite element models were used. Although both analyses predicted similar overall creep rates, three-dimensional stress analysis was required to obtain detailed information about the stress state in the vicinity of the fibre-matrix interface. The results of the analysis indicate that the tensile radial stress, which develops in the vicinity of the fibre-matrix interface after processing, rapidly decreases during the initial stages of creep. Both the predicted and experimental results for the composite show that 50% of the total creep strain which accumulated after 200 h at a stress of 200 MPa and temperature of 1200°C is recovered within 25 h of unloading. Residual Stress Creep Rate Creep Strain Creep Deformation Creep Property Holmes, J. W. aut Enthalten in Journal of materials science Kluwer Academic Publishers-Plenum Publishers, 1966 27(1992), 23 vom: 01. Jan., Seite 6341-6351 (DE-627)129546372 (DE-600)218324-9 (DE-576)014996774 0022-2461 nnns volume:27 year:1992 number:23 day:01 month:01 pages:6341-6351 https://doi.org/10.1007/BF00576283 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_OLC SSG-OLC-TEC GBV_ILN_11 GBV_ILN_20 GBV_ILN_23 GBV_ILN_30 GBV_ILN_32 GBV_ILN_40 GBV_ILN_62 GBV_ILN_65 GBV_ILN_70 GBV_ILN_2004 GBV_ILN_2006 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_4082 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4316 GBV_ILN_4319 GBV_ILN_4323 GBV_ILN_4700 AR 27 1992 23 01 01 6341-6351
language	English
source	Enthalten in Journal of materials science 27(1992), 23 vom: 01. Jan., Seite 6341-6351 volume:27 year:1992 number:23 day:01 month:01 pages:6341-6351
sourceStr	Enthalten in Journal of materials science 27(1992), 23 vom: 01. Jan., Seite 6341-6351 volume:27 year:1992 number:23 day:01 month:01 pages:6341-6351
format_phy_str_mv	Article
institution	findex.gbv.de
topic_facet	Residual Stress Creep Rate Creep Strain Creep Deformation Creep Property
dewey-raw	670
isfreeaccess_bool	false
container_title	Journal of materials science
authorswithroles_txt_mv	Park, Y. H. @@aut@@ Holmes, J. W. @@aut@@
publishDateDaySort_date	1992-01-01T00:00:00Z
hierarchy_top_id	129546372
dewey-sort	3670
id	OLC2046194926
language_de	englisch
fullrecord	<?xml version="1.0" encoding="UTF-8"?><collection xmlns="http://www.loc.gov/MARC21/slim"><record><leader>01000caa a22002652 4500</leader><controlfield tag="001">OLC2046194926</controlfield><controlfield tag="003">DE-627</controlfield><controlfield tag="005">20230503122250.0</controlfield><controlfield tag="007">tu</controlfield><controlfield tag="008">200820s1992 xx \|\|\|\|\| 00\| \|\|eng c</controlfield><datafield tag="024" ind1="7" ind2=" "><subfield code="a">10.1007/BF00576283</subfield><subfield code="2">doi</subfield></datafield><datafield tag="035" ind1=" " ind2=" "><subfield code="a">(DE-627)OLC2046194926</subfield></datafield><datafield tag="035" ind1=" " ind2=" "><subfield code="a">(DE-He213)BF00576283-p</subfield></datafield><datafield tag="040" ind1=" " ind2=" "><subfield code="a">DE-627</subfield><subfield code="b">ger</subfield><subfield code="c">DE-627</subfield><subfield code="e">rakwb</subfield></datafield><datafield tag="041" ind1=" " ind2=" "><subfield code="a">eng</subfield></datafield><datafield tag="082" ind1="0" ind2="4"><subfield code="a">670</subfield><subfield code="q">VZ</subfield></datafield><datafield tag="100" ind1="1" ind2=" "><subfield code="a">Park, Y. H.</subfield><subfield code="e">verfasserin</subfield><subfield code="4">aut</subfield></datafield><datafield tag="245" ind1="1" ind2="0"><subfield code="a">Finite element modelling of creep deformation in fibre-reinforced ceramic composites</subfield></datafield><datafield tag="264" ind1=" " ind2="1"><subfield code="c">1992</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">ohne Hilfsmittel zu benutzen</subfield><subfield code="b">n</subfield><subfield code="2">rdamedia</subfield></datafield><datafield tag="338" ind1=" " ind2=" "><subfield code="a">Band</subfield><subfield code="b">nc</subfield><subfield code="2">rdacarrier</subfield></datafield><datafield tag="500" ind1=" " ind2=" "><subfield code="a">© Chapman & Hall 1992</subfield></datafield><datafield tag="520" ind1=" " ind2=" "><subfield code="a">Abstract The tensile creep and creep-recovery behaviour of a unidirectional SiC fibre-$ Si_{3} $$ N_{4} $ matrix composite was analysed using finite element techniques. The analysis, based on the elastic and creep properties of each constituent, considered the influence of fibre-matrix bonding and processing-related residual stresses on creep and creep-recovery behaviour. Both two- and three-dimensional finite element models were used. Although both analyses predicted similar overall creep rates, three-dimensional stress analysis was required to obtain detailed information about the stress state in the vicinity of the fibre-matrix interface. The results of the analysis indicate that the tensile radial stress, which develops in the vicinity of the fibre-matrix interface after processing, rapidly decreases during the initial stages of creep. Both the predicted and experimental results for the composite show that 50% of the total creep strain which accumulated after 200 h at a stress of 200 MPa and temperature of 1200°C is recovered within 25 h of unloading.</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Residual Stress</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Creep Rate</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Creep Strain</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Creep Deformation</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Creep Property</subfield></datafield><datafield tag="700" ind1="1" ind2=" "><subfield code="a">Holmes, J. W.</subfield><subfield code="4">aut</subfield></datafield><datafield tag="773" ind1="0" ind2="8"><subfield code="i">Enthalten in</subfield><subfield code="t">Journal of materials science</subfield><subfield code="d">Kluwer Academic Publishers-Plenum Publishers, 1966</subfield><subfield code="g">27(1992), 23 vom: 01. Jan., Seite 6341-6351</subfield><subfield code="w">(DE-627)129546372</subfield><subfield code="w">(DE-600)218324-9</subfield><subfield code="w">(DE-576)014996774</subfield><subfield code="x">0022-2461</subfield><subfield code="7">nnns</subfield></datafield><datafield tag="773" ind1="1" ind2="8"><subfield code="g">volume:27</subfield><subfield code="g">year:1992</subfield><subfield code="g">number:23</subfield><subfield code="g">day:01</subfield><subfield code="g">month:01</subfield><subfield code="g">pages:6341-6351</subfield></datafield><datafield tag="856" ind1="4" ind2="1"><subfield code="u">https://doi.org/10.1007/BF00576283</subfield><subfield code="z">lizenzpflichtig</subfield><subfield code="3">Volltext</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_USEFLAG_A</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">SYSFLAG_A</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_OLC</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">SSG-OLC-TEC</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_11</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_20</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_23</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_30</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_32</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_40</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_62</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_65</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_70</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_2004</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_2006</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_2015</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_2020</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_2021</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_4082</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_4305</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_4306</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_4316</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_4319</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_4323</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_4700</subfield></datafield><datafield tag="951" ind1=" " ind2=" "><subfield code="a">AR</subfield></datafield><datafield tag="952" ind1=" " ind2=" "><subfield code="d">27</subfield><subfield code="j">1992</subfield><subfield code="e">23</subfield><subfield code="b">01</subfield><subfield code="c">01</subfield><subfield code="h">6341-6351</subfield></datafield></record></collection>
author	Park, Y. H.
spellingShingle	Park, Y. H. ddc 670 misc Residual Stress misc Creep Rate misc Creep Strain misc Creep Deformation misc Creep Property Finite element modelling of creep deformation in fibre-reinforced ceramic composites
authorStr	Park, Y. H.
ppnlink_with_tag_str_mv	@@773@@(DE-627)129546372
format	Article
dewey-ones	670 - Manufacturing
delete_txt_mv	keep
author_role	aut aut
collection	OLC
remote_str	false
illustrated	Not Illustrated
issn	0022-2461
topic_title	670 VZ Finite element modelling of creep deformation in fibre-reinforced ceramic composites Residual Stress Creep Rate Creep Strain Creep Deformation Creep Property
topic	ddc 670 misc Residual Stress misc Creep Rate misc Creep Strain misc Creep Deformation misc Creep Property
topic_unstemmed	ddc 670 misc Residual Stress misc Creep Rate misc Creep Strain misc Creep Deformation misc Creep Property
topic_browse	ddc 670 misc Residual Stress misc Creep Rate misc Creep Strain misc Creep Deformation misc Creep Property
format_facet	Aufsätze Gedruckte Aufsätze
format_main_str_mv	Text Zeitschrift/Artikel
carriertype_str_mv	nc
hierarchy_parent_title	Journal of materials science
hierarchy_parent_id	129546372
dewey-tens	670 - Manufacturing
hierarchy_top_title	Journal of materials science
isfreeaccess_txt	false
familylinks_str_mv	(DE-627)129546372 (DE-600)218324-9 (DE-576)014996774
title	Finite element modelling of creep deformation in fibre-reinforced ceramic composites
ctrlnum	(DE-627)OLC2046194926 (DE-He213)BF00576283-p
title_full	Finite element modelling of creep deformation in fibre-reinforced ceramic composites
author_sort	Park, Y. H.
journal	Journal of materials science
journalStr	Journal of materials science
lang_code	eng
isOA_bool	false
dewey-hundreds	600 - Technology
recordtype	marc
publishDateSort	1992
contenttype_str_mv	txt
container_start_page	6341
author_browse	Park, Y. H. Holmes, J. W.
container_volume	27
class	670 VZ
format_se	Aufsätze
author-letter	Park, Y. H.
doi_str_mv	10.1007/BF00576283
dewey-full	670
title_sort	finite element modelling of creep deformation in fibre-reinforced ceramic composites
title_auth	Finite element modelling of creep deformation in fibre-reinforced ceramic composites
abstract	Abstract The tensile creep and creep-recovery behaviour of a unidirectional SiC fibre-$ Si_{3} $$ N_{4} $ matrix composite was analysed using finite element techniques. The analysis, based on the elastic and creep properties of each constituent, considered the influence of fibre-matrix bonding and processing-related residual stresses on creep and creep-recovery behaviour. Both two- and three-dimensional finite element models were used. Although both analyses predicted similar overall creep rates, three-dimensional stress analysis was required to obtain detailed information about the stress state in the vicinity of the fibre-matrix interface. The results of the analysis indicate that the tensile radial stress, which develops in the vicinity of the fibre-matrix interface after processing, rapidly decreases during the initial stages of creep. Both the predicted and experimental results for the composite show that 50% of the total creep strain which accumulated after 200 h at a stress of 200 MPa and temperature of 1200°C is recovered within 25 h of unloading. © Chapman & Hall 1992
abstractGer	Abstract The tensile creep and creep-recovery behaviour of a unidirectional SiC fibre-$ Si_{3} $$ N_{4} $ matrix composite was analysed using finite element techniques. The analysis, based on the elastic and creep properties of each constituent, considered the influence of fibre-matrix bonding and processing-related residual stresses on creep and creep-recovery behaviour. Both two- and three-dimensional finite element models were used. Although both analyses predicted similar overall creep rates, three-dimensional stress analysis was required to obtain detailed information about the stress state in the vicinity of the fibre-matrix interface. The results of the analysis indicate that the tensile radial stress, which develops in the vicinity of the fibre-matrix interface after processing, rapidly decreases during the initial stages of creep. Both the predicted and experimental results for the composite show that 50% of the total creep strain which accumulated after 200 h at a stress of 200 MPa and temperature of 1200°C is recovered within 25 h of unloading. © Chapman & Hall 1992
abstract_unstemmed	Abstract The tensile creep and creep-recovery behaviour of a unidirectional SiC fibre-$ Si_{3} $$ N_{4} $ matrix composite was analysed using finite element techniques. The analysis, based on the elastic and creep properties of each constituent, considered the influence of fibre-matrix bonding and processing-related residual stresses on creep and creep-recovery behaviour. Both two- and three-dimensional finite element models were used. Although both analyses predicted similar overall creep rates, three-dimensional stress analysis was required to obtain detailed information about the stress state in the vicinity of the fibre-matrix interface. The results of the analysis indicate that the tensile radial stress, which develops in the vicinity of the fibre-matrix interface after processing, rapidly decreases during the initial stages of creep. Both the predicted and experimental results for the composite show that 50% of the total creep strain which accumulated after 200 h at a stress of 200 MPa and temperature of 1200°C is recovered within 25 h of unloading. © Chapman & Hall 1992
collection_details	GBV_USEFLAG_A SYSFLAG_A GBV_OLC SSG-OLC-TEC GBV_ILN_11 GBV_ILN_20 GBV_ILN_23 GBV_ILN_30 GBV_ILN_32 GBV_ILN_40 GBV_ILN_62 GBV_ILN_65 GBV_ILN_70 GBV_ILN_2004 GBV_ILN_2006 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_4082 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4316 GBV_ILN_4319 GBV_ILN_4323 GBV_ILN_4700
container_issue	23
title_short	Finite element modelling of creep deformation in fibre-reinforced ceramic composites
url	https://doi.org/10.1007/BF00576283
remote_bool	false
author2	Holmes, J. W.
author2Str	Holmes, J. W.
ppnlink	129546372
mediatype_str_mv	n
isOA_txt	false
hochschulschrift_bool	false
doi_str	10.1007/BF00576283
up_date	2024-07-04T04:28:42.333Z
_version_	1803621312584744961
fullrecord_marcxml	<?xml version="1.0" encoding="UTF-8"?><collection xmlns="http://www.loc.gov/MARC21/slim"><record><leader>01000caa a22002652 4500</leader><controlfield tag="001">OLC2046194926</controlfield><controlfield tag="003">DE-627</controlfield><controlfield tag="005">20230503122250.0</controlfield><controlfield tag="007">tu</controlfield><controlfield tag="008">200820s1992 xx \|\|\|\|\| 00\| \|\|eng c</controlfield><datafield tag="024" ind1="7" ind2=" "><subfield code="a">10.1007/BF00576283</subfield><subfield code="2">doi</subfield></datafield><datafield tag="035" ind1=" " ind2=" "><subfield code="a">(DE-627)OLC2046194926</subfield></datafield><datafield tag="035" ind1=" " ind2=" "><subfield code="a">(DE-He213)BF00576283-p</subfield></datafield><datafield tag="040" ind1=" " ind2=" "><subfield code="a">DE-627</subfield><subfield code="b">ger</subfield><subfield code="c">DE-627</subfield><subfield code="e">rakwb</subfield></datafield><datafield tag="041" ind1=" " ind2=" "><subfield code="a">eng</subfield></datafield><datafield tag="082" ind1="0" ind2="4"><subfield code="a">670</subfield><subfield code="q">VZ</subfield></datafield><datafield tag="100" ind1="1" ind2=" "><subfield code="a">Park, Y. H.</subfield><subfield code="e">verfasserin</subfield><subfield code="4">aut</subfield></datafield><datafield tag="245" ind1="1" ind2="0"><subfield code="a">Finite element modelling of creep deformation in fibre-reinforced ceramic composites</subfield></datafield><datafield tag="264" ind1=" " ind2="1"><subfield code="c">1992</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">ohne Hilfsmittel zu benutzen</subfield><subfield code="b">n</subfield><subfield code="2">rdamedia</subfield></datafield><datafield tag="338" ind1=" " ind2=" "><subfield code="a">Band</subfield><subfield code="b">nc</subfield><subfield code="2">rdacarrier</subfield></datafield><datafield tag="500" ind1=" " ind2=" "><subfield code="a">© Chapman & Hall 1992</subfield></datafield><datafield tag="520" ind1=" " ind2=" "><subfield code="a">Abstract The tensile creep and creep-recovery behaviour of a unidirectional SiC fibre-$ Si_{3} $$ N_{4} $ matrix composite was analysed using finite element techniques. The analysis, based on the elastic and creep properties of each constituent, considered the influence of fibre-matrix bonding and processing-related residual stresses on creep and creep-recovery behaviour. Both two- and three-dimensional finite element models were used. Although both analyses predicted similar overall creep rates, three-dimensional stress analysis was required to obtain detailed information about the stress state in the vicinity of the fibre-matrix interface. The results of the analysis indicate that the tensile radial stress, which develops in the vicinity of the fibre-matrix interface after processing, rapidly decreases during the initial stages of creep. Both the predicted and experimental results for the composite show that 50% of the total creep strain which accumulated after 200 h at a stress of 200 MPa and temperature of 1200°C is recovered within 25 h of unloading.</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Residual Stress</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Creep Rate</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Creep Strain</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Creep Deformation</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Creep Property</subfield></datafield><datafield tag="700" ind1="1" ind2=" "><subfield code="a">Holmes, J. W.</subfield><subfield code="4">aut</subfield></datafield><datafield tag="773" ind1="0" ind2="8"><subfield code="i">Enthalten in</subfield><subfield code="t">Journal of materials science</subfield><subfield code="d">Kluwer Academic Publishers-Plenum Publishers, 1966</subfield><subfield code="g">27(1992), 23 vom: 01. Jan., Seite 6341-6351</subfield><subfield code="w">(DE-627)129546372</subfield><subfield code="w">(DE-600)218324-9</subfield><subfield code="w">(DE-576)014996774</subfield><subfield code="x">0022-2461</subfield><subfield code="7">nnns</subfield></datafield><datafield tag="773" ind1="1" ind2="8"><subfield code="g">volume:27</subfield><subfield code="g">year:1992</subfield><subfield code="g">number:23</subfield><subfield code="g">day:01</subfield><subfield code="g">month:01</subfield><subfield code="g">pages:6341-6351</subfield></datafield><datafield tag="856" ind1="4" ind2="1"><subfield code="u">https://doi.org/10.1007/BF00576283</subfield><subfield code="z">lizenzpflichtig</subfield><subfield code="3">Volltext</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_USEFLAG_A</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">SYSFLAG_A</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_OLC</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">SSG-OLC-TEC</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_11</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_20</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_23</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_30</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_32</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_40</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_62</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_65</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_70</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_2004</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_2006</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_2015</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_2020</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_2021</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_4082</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_4305</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_4306</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_4316</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_4319</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_4323</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_4700</subfield></datafield><datafield tag="951" ind1=" " ind2=" "><subfield code="a">AR</subfield></datafield><datafield tag="952" ind1=" " ind2=" "><subfield code="d">27</subfield><subfield code="j">1992</subfield><subfield code="e">23</subfield><subfield code="b">01</subfield><subfield code="c">01</subfield><subfield code="h">6341-6351</subfield></datafield></record></collection>
score	7.4011316

Nicht das Richtige dabei?

Schreiben Sie uns!

Finite element modelling of creep deformation in fibre-reinforced ceramic composites

Nicht das Richtige dabei?

Zugang & Verfügbarkeit

Vorhandene Bände

Nicht das Richtige dabei?