On stress propagation and fracture in compacted graphite iron
Abstract In this work, initiation and propagation of fracture in compacted graphite iron (CGI) has been investigated and modeled under the dynamic loading scenario. Fracture initiation was found to originate at the graphite particles and at graphite/matrix interface at no particular preference of or...
Ausführliche Beschreibung
Autor*in: |
Mohammed, Walid M. [verfasserIn] |
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Format: |
E-Artikel |
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Sprache: |
Englisch |
Erschienen: |
2011 |
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Schlagwörter: |
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Anmerkung: |
© Springer-Verlag London Limited 2011 |
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Übergeordnetes Werk: |
Enthalten in: The international journal of advanced manufacturing technology - London : Springer, 1985, 56(2011), 1-4 vom: 22. Jan., Seite 233-244 |
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Übergeordnetes Werk: |
volume:56 ; year:2011 ; number:1-4 ; day:22 ; month:01 ; pages:233-244 |
Links: |
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DOI / URN: |
10.1007/s00170-011-3157-1 |
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Katalog-ID: |
SPR001679457 |
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520 | |a Abstract In this work, initiation and propagation of fracture in compacted graphite iron (CGI) has been investigated and modeled under the dynamic loading scenario. Fracture initiation was found to originate at the graphite particles and at graphite/matrix interface at no particular preference of order and propagated into the metal matrix in the form of a network of microcracks which eventually coalesced leading to complete failure of the material. Metallurgical investigations of fracture in CGI under both quasi-static and quasi-dynamic tests were comprehensively implemented. Investigation of stress concentration propagation at specific fracture propensity regions have been modeled and simulated on a real CGI sample RVE using commercial finite element package, ABAQUS™/CAE™ v6.9. The CGI sample consisted of >90% pearlite matrix. Furthermore, FE modeling allowed the observation of stress concentration initiation and propagation at the CGI graphite particles and graphite–matrix interfaces until fracture. Crack bluntness was observed in the model and a change in the potential crack path was visual. Several findings were documented in an effort to better understand the behavior of CGI under quasi-static and dynamic conditions. This work is a milestone among a series of successive tasks all aiming to better understand, validate, and build a yet unavailable comprehensive model of CGI behavior under diverse loading schemes. | ||
650 | 4 | |a Compacted graphite iron |7 (dpeaa)DE-He213 | |
650 | 4 | |a Fracture |7 (dpeaa)DE-He213 | |
650 | 4 | |a Finite element analysis (FEA) |7 (dpeaa)DE-He213 | |
700 | 1 | |a Ng, Eu-Gene |4 aut | |
700 | 1 | |a Elbestawi, M. A. |4 aut | |
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10.1007/s00170-011-3157-1 doi (DE-627)SPR001679457 (SPR)s00170-011-3157-1-e DE-627 ger DE-627 rakwb eng Mohammed, Walid M. verfasserin aut On stress propagation and fracture in compacted graphite iron 2011 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier © Springer-Verlag London Limited 2011 Abstract In this work, initiation and propagation of fracture in compacted graphite iron (CGI) has been investigated and modeled under the dynamic loading scenario. Fracture initiation was found to originate at the graphite particles and at graphite/matrix interface at no particular preference of order and propagated into the metal matrix in the form of a network of microcracks which eventually coalesced leading to complete failure of the material. Metallurgical investigations of fracture in CGI under both quasi-static and quasi-dynamic tests were comprehensively implemented. Investigation of stress concentration propagation at specific fracture propensity regions have been modeled and simulated on a real CGI sample RVE using commercial finite element package, ABAQUS™/CAE™ v6.9. The CGI sample consisted of >90% pearlite matrix. Furthermore, FE modeling allowed the observation of stress concentration initiation and propagation at the CGI graphite particles and graphite–matrix interfaces until fracture. Crack bluntness was observed in the model and a change in the potential crack path was visual. Several findings were documented in an effort to better understand the behavior of CGI under quasi-static and dynamic conditions. This work is a milestone among a series of successive tasks all aiming to better understand, validate, and build a yet unavailable comprehensive model of CGI behavior under diverse loading schemes. Compacted graphite iron (dpeaa)DE-He213 Fracture (dpeaa)DE-He213 Finite element analysis (FEA) (dpeaa)DE-He213 Ng, Eu-Gene aut Elbestawi, M. A. aut Enthalten in The international journal of advanced manufacturing technology London : Springer, 1985 56(2011), 1-4 vom: 22. Jan., Seite 233-244 (DE-627)270127712 (DE-600)1476510-X 1433-3015 nnns volume:56 year:2011 number:1-4 day:22 month:01 pages:233-244 https://dx.doi.org/10.1007/s00170-011-3157-1 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_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_206 GBV_ILN_213 GBV_ILN_224 GBV_ILN_230 GBV_ILN_250 GBV_ILN_281 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_636 GBV_ILN_702 GBV_ILN_2001 GBV_ILN_2003 GBV_ILN_2004 GBV_ILN_2005 GBV_ILN_2006 GBV_ILN_2007 GBV_ILN_2008 GBV_ILN_2009 GBV_ILN_2010 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_2025 GBV_ILN_2026 GBV_ILN_2027 GBV_ILN_2031 GBV_ILN_2034 GBV_ILN_2037 GBV_ILN_2038 GBV_ILN_2039 GBV_ILN_2044 GBV_ILN_2048 GBV_ILN_2049 GBV_ILN_2050 GBV_ILN_2055 GBV_ILN_2056 GBV_ILN_2057 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 GBV_ILN_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 56 2011 1-4 22 01 233-244 |
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10.1007/s00170-011-3157-1 doi (DE-627)SPR001679457 (SPR)s00170-011-3157-1-e DE-627 ger DE-627 rakwb eng Mohammed, Walid M. verfasserin aut On stress propagation and fracture in compacted graphite iron 2011 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier © Springer-Verlag London Limited 2011 Abstract In this work, initiation and propagation of fracture in compacted graphite iron (CGI) has been investigated and modeled under the dynamic loading scenario. Fracture initiation was found to originate at the graphite particles and at graphite/matrix interface at no particular preference of order and propagated into the metal matrix in the form of a network of microcracks which eventually coalesced leading to complete failure of the material. Metallurgical investigations of fracture in CGI under both quasi-static and quasi-dynamic tests were comprehensively implemented. Investigation of stress concentration propagation at specific fracture propensity regions have been modeled and simulated on a real CGI sample RVE using commercial finite element package, ABAQUS™/CAE™ v6.9. The CGI sample consisted of >90% pearlite matrix. Furthermore, FE modeling allowed the observation of stress concentration initiation and propagation at the CGI graphite particles and graphite–matrix interfaces until fracture. Crack bluntness was observed in the model and a change in the potential crack path was visual. Several findings were documented in an effort to better understand the behavior of CGI under quasi-static and dynamic conditions. This work is a milestone among a series of successive tasks all aiming to better understand, validate, and build a yet unavailable comprehensive model of CGI behavior under diverse loading schemes. Compacted graphite iron (dpeaa)DE-He213 Fracture (dpeaa)DE-He213 Finite element analysis (FEA) (dpeaa)DE-He213 Ng, Eu-Gene aut Elbestawi, M. A. aut Enthalten in The international journal of advanced manufacturing technology London : Springer, 1985 56(2011), 1-4 vom: 22. Jan., Seite 233-244 (DE-627)270127712 (DE-600)1476510-X 1433-3015 nnns volume:56 year:2011 number:1-4 day:22 month:01 pages:233-244 https://dx.doi.org/10.1007/s00170-011-3157-1 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_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_206 GBV_ILN_213 GBV_ILN_224 GBV_ILN_230 GBV_ILN_250 GBV_ILN_281 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_636 GBV_ILN_702 GBV_ILN_2001 GBV_ILN_2003 GBV_ILN_2004 GBV_ILN_2005 GBV_ILN_2006 GBV_ILN_2007 GBV_ILN_2008 GBV_ILN_2009 GBV_ILN_2010 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_2025 GBV_ILN_2026 GBV_ILN_2027 GBV_ILN_2031 GBV_ILN_2034 GBV_ILN_2037 GBV_ILN_2038 GBV_ILN_2039 GBV_ILN_2044 GBV_ILN_2048 GBV_ILN_2049 GBV_ILN_2050 GBV_ILN_2055 GBV_ILN_2056 GBV_ILN_2057 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 GBV_ILN_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 56 2011 1-4 22 01 233-244 |
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10.1007/s00170-011-3157-1 doi (DE-627)SPR001679457 (SPR)s00170-011-3157-1-e DE-627 ger DE-627 rakwb eng Mohammed, Walid M. verfasserin aut On stress propagation and fracture in compacted graphite iron 2011 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier © Springer-Verlag London Limited 2011 Abstract In this work, initiation and propagation of fracture in compacted graphite iron (CGI) has been investigated and modeled under the dynamic loading scenario. Fracture initiation was found to originate at the graphite particles and at graphite/matrix interface at no particular preference of order and propagated into the metal matrix in the form of a network of microcracks which eventually coalesced leading to complete failure of the material. Metallurgical investigations of fracture in CGI under both quasi-static and quasi-dynamic tests were comprehensively implemented. Investigation of stress concentration propagation at specific fracture propensity regions have been modeled and simulated on a real CGI sample RVE using commercial finite element package, ABAQUS™/CAE™ v6.9. The CGI sample consisted of >90% pearlite matrix. Furthermore, FE modeling allowed the observation of stress concentration initiation and propagation at the CGI graphite particles and graphite–matrix interfaces until fracture. Crack bluntness was observed in the model and a change in the potential crack path was visual. Several findings were documented in an effort to better understand the behavior of CGI under quasi-static and dynamic conditions. This work is a milestone among a series of successive tasks all aiming to better understand, validate, and build a yet unavailable comprehensive model of CGI behavior under diverse loading schemes. Compacted graphite iron (dpeaa)DE-He213 Fracture (dpeaa)DE-He213 Finite element analysis (FEA) (dpeaa)DE-He213 Ng, Eu-Gene aut Elbestawi, M. A. aut Enthalten in The international journal of advanced manufacturing technology London : Springer, 1985 56(2011), 1-4 vom: 22. Jan., Seite 233-244 (DE-627)270127712 (DE-600)1476510-X 1433-3015 nnns volume:56 year:2011 number:1-4 day:22 month:01 pages:233-244 https://dx.doi.org/10.1007/s00170-011-3157-1 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_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_206 GBV_ILN_213 GBV_ILN_224 GBV_ILN_230 GBV_ILN_250 GBV_ILN_281 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_636 GBV_ILN_702 GBV_ILN_2001 GBV_ILN_2003 GBV_ILN_2004 GBV_ILN_2005 GBV_ILN_2006 GBV_ILN_2007 GBV_ILN_2008 GBV_ILN_2009 GBV_ILN_2010 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_2025 GBV_ILN_2026 GBV_ILN_2027 GBV_ILN_2031 GBV_ILN_2034 GBV_ILN_2037 GBV_ILN_2038 GBV_ILN_2039 GBV_ILN_2044 GBV_ILN_2048 GBV_ILN_2049 GBV_ILN_2050 GBV_ILN_2055 GBV_ILN_2056 GBV_ILN_2057 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 GBV_ILN_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 56 2011 1-4 22 01 233-244 |
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10.1007/s00170-011-3157-1 doi (DE-627)SPR001679457 (SPR)s00170-011-3157-1-e DE-627 ger DE-627 rakwb eng Mohammed, Walid M. verfasserin aut On stress propagation and fracture in compacted graphite iron 2011 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier © Springer-Verlag London Limited 2011 Abstract In this work, initiation and propagation of fracture in compacted graphite iron (CGI) has been investigated and modeled under the dynamic loading scenario. Fracture initiation was found to originate at the graphite particles and at graphite/matrix interface at no particular preference of order and propagated into the metal matrix in the form of a network of microcracks which eventually coalesced leading to complete failure of the material. Metallurgical investigations of fracture in CGI under both quasi-static and quasi-dynamic tests were comprehensively implemented. Investigation of stress concentration propagation at specific fracture propensity regions have been modeled and simulated on a real CGI sample RVE using commercial finite element package, ABAQUS™/CAE™ v6.9. The CGI sample consisted of >90% pearlite matrix. Furthermore, FE modeling allowed the observation of stress concentration initiation and propagation at the CGI graphite particles and graphite–matrix interfaces until fracture. Crack bluntness was observed in the model and a change in the potential crack path was visual. Several findings were documented in an effort to better understand the behavior of CGI under quasi-static and dynamic conditions. This work is a milestone among a series of successive tasks all aiming to better understand, validate, and build a yet unavailable comprehensive model of CGI behavior under diverse loading schemes. Compacted graphite iron (dpeaa)DE-He213 Fracture (dpeaa)DE-He213 Finite element analysis (FEA) (dpeaa)DE-He213 Ng, Eu-Gene aut Elbestawi, M. A. aut Enthalten in The international journal of advanced manufacturing technology London : Springer, 1985 56(2011), 1-4 vom: 22. Jan., Seite 233-244 (DE-627)270127712 (DE-600)1476510-X 1433-3015 nnns volume:56 year:2011 number:1-4 day:22 month:01 pages:233-244 https://dx.doi.org/10.1007/s00170-011-3157-1 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_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_206 GBV_ILN_213 GBV_ILN_224 GBV_ILN_230 GBV_ILN_250 GBV_ILN_281 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_636 GBV_ILN_702 GBV_ILN_2001 GBV_ILN_2003 GBV_ILN_2004 GBV_ILN_2005 GBV_ILN_2006 GBV_ILN_2007 GBV_ILN_2008 GBV_ILN_2009 GBV_ILN_2010 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_2025 GBV_ILN_2026 GBV_ILN_2027 GBV_ILN_2031 GBV_ILN_2034 GBV_ILN_2037 GBV_ILN_2038 GBV_ILN_2039 GBV_ILN_2044 GBV_ILN_2048 GBV_ILN_2049 GBV_ILN_2050 GBV_ILN_2055 GBV_ILN_2056 GBV_ILN_2057 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 GBV_ILN_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 56 2011 1-4 22 01 233-244 |
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10.1007/s00170-011-3157-1 doi (DE-627)SPR001679457 (SPR)s00170-011-3157-1-e DE-627 ger DE-627 rakwb eng Mohammed, Walid M. verfasserin aut On stress propagation and fracture in compacted graphite iron 2011 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier © Springer-Verlag London Limited 2011 Abstract In this work, initiation and propagation of fracture in compacted graphite iron (CGI) has been investigated and modeled under the dynamic loading scenario. Fracture initiation was found to originate at the graphite particles and at graphite/matrix interface at no particular preference of order and propagated into the metal matrix in the form of a network of microcracks which eventually coalesced leading to complete failure of the material. Metallurgical investigations of fracture in CGI under both quasi-static and quasi-dynamic tests were comprehensively implemented. Investigation of stress concentration propagation at specific fracture propensity regions have been modeled and simulated on a real CGI sample RVE using commercial finite element package, ABAQUS™/CAE™ v6.9. The CGI sample consisted of >90% pearlite matrix. Furthermore, FE modeling allowed the observation of stress concentration initiation and propagation at the CGI graphite particles and graphite–matrix interfaces until fracture. Crack bluntness was observed in the model and a change in the potential crack path was visual. Several findings were documented in an effort to better understand the behavior of CGI under quasi-static and dynamic conditions. This work is a milestone among a series of successive tasks all aiming to better understand, validate, and build a yet unavailable comprehensive model of CGI behavior under diverse loading schemes. Compacted graphite iron (dpeaa)DE-He213 Fracture (dpeaa)DE-He213 Finite element analysis (FEA) (dpeaa)DE-He213 Ng, Eu-Gene aut Elbestawi, M. A. aut Enthalten in The international journal of advanced manufacturing technology London : Springer, 1985 56(2011), 1-4 vom: 22. Jan., Seite 233-244 (DE-627)270127712 (DE-600)1476510-X 1433-3015 nnns volume:56 year:2011 number:1-4 day:22 month:01 pages:233-244 https://dx.doi.org/10.1007/s00170-011-3157-1 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_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_206 GBV_ILN_213 GBV_ILN_224 GBV_ILN_230 GBV_ILN_250 GBV_ILN_281 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_636 GBV_ILN_702 GBV_ILN_2001 GBV_ILN_2003 GBV_ILN_2004 GBV_ILN_2005 GBV_ILN_2006 GBV_ILN_2007 GBV_ILN_2008 GBV_ILN_2009 GBV_ILN_2010 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_2025 GBV_ILN_2026 GBV_ILN_2027 GBV_ILN_2031 GBV_ILN_2034 GBV_ILN_2037 GBV_ILN_2038 GBV_ILN_2039 GBV_ILN_2044 GBV_ILN_2048 GBV_ILN_2049 GBV_ILN_2050 GBV_ILN_2055 GBV_ILN_2056 GBV_ILN_2057 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 GBV_ILN_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 56 2011 1-4 22 01 233-244 |
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Mohammed, Walid M. |
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on stress propagation and fracture in compacted graphite iron |
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On stress propagation and fracture in compacted graphite iron |
abstract |
Abstract In this work, initiation and propagation of fracture in compacted graphite iron (CGI) has been investigated and modeled under the dynamic loading scenario. Fracture initiation was found to originate at the graphite particles and at graphite/matrix interface at no particular preference of order and propagated into the metal matrix in the form of a network of microcracks which eventually coalesced leading to complete failure of the material. Metallurgical investigations of fracture in CGI under both quasi-static and quasi-dynamic tests were comprehensively implemented. Investigation of stress concentration propagation at specific fracture propensity regions have been modeled and simulated on a real CGI sample RVE using commercial finite element package, ABAQUS™/CAE™ v6.9. The CGI sample consisted of >90% pearlite matrix. Furthermore, FE modeling allowed the observation of stress concentration initiation and propagation at the CGI graphite particles and graphite–matrix interfaces until fracture. Crack bluntness was observed in the model and a change in the potential crack path was visual. Several findings were documented in an effort to better understand the behavior of CGI under quasi-static and dynamic conditions. This work is a milestone among a series of successive tasks all aiming to better understand, validate, and build a yet unavailable comprehensive model of CGI behavior under diverse loading schemes. © Springer-Verlag London Limited 2011 |
abstractGer |
Abstract In this work, initiation and propagation of fracture in compacted graphite iron (CGI) has been investigated and modeled under the dynamic loading scenario. Fracture initiation was found to originate at the graphite particles and at graphite/matrix interface at no particular preference of order and propagated into the metal matrix in the form of a network of microcracks which eventually coalesced leading to complete failure of the material. Metallurgical investigations of fracture in CGI under both quasi-static and quasi-dynamic tests were comprehensively implemented. Investigation of stress concentration propagation at specific fracture propensity regions have been modeled and simulated on a real CGI sample RVE using commercial finite element package, ABAQUS™/CAE™ v6.9. The CGI sample consisted of >90% pearlite matrix. Furthermore, FE modeling allowed the observation of stress concentration initiation and propagation at the CGI graphite particles and graphite–matrix interfaces until fracture. Crack bluntness was observed in the model and a change in the potential crack path was visual. Several findings were documented in an effort to better understand the behavior of CGI under quasi-static and dynamic conditions. This work is a milestone among a series of successive tasks all aiming to better understand, validate, and build a yet unavailable comprehensive model of CGI behavior under diverse loading schemes. © Springer-Verlag London Limited 2011 |
abstract_unstemmed |
Abstract In this work, initiation and propagation of fracture in compacted graphite iron (CGI) has been investigated and modeled under the dynamic loading scenario. Fracture initiation was found to originate at the graphite particles and at graphite/matrix interface at no particular preference of order and propagated into the metal matrix in the form of a network of microcracks which eventually coalesced leading to complete failure of the material. Metallurgical investigations of fracture in CGI under both quasi-static and quasi-dynamic tests were comprehensively implemented. Investigation of stress concentration propagation at specific fracture propensity regions have been modeled and simulated on a real CGI sample RVE using commercial finite element package, ABAQUS™/CAE™ v6.9. The CGI sample consisted of >90% pearlite matrix. Furthermore, FE modeling allowed the observation of stress concentration initiation and propagation at the CGI graphite particles and graphite–matrix interfaces until fracture. Crack bluntness was observed in the model and a change in the potential crack path was visual. Several findings were documented in an effort to better understand the behavior of CGI under quasi-static and dynamic conditions. This work is a milestone among a series of successive tasks all aiming to better understand, validate, and build a yet unavailable comprehensive model of CGI behavior under diverse loading schemes. © Springer-Verlag London Limited 2011 |
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title_short |
On stress propagation and fracture in compacted graphite iron |
url |
https://dx.doi.org/10.1007/s00170-011-3157-1 |
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author2 |
Ng, Eu-Gene Elbestawi, M. A. |
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Ng, Eu-Gene Elbestawi, M. A. |
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10.1007/s00170-011-3157-1 |
up_date |
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