Effect of FDM process parameters on mechanical properties of 3D-printed carbon fibre–PLA composite
Abstract This paper presents the effect of process parameters of the fused deposition modelling (FDM) method on mechanical properties of 3D-printed carbon fibre (CF)-reinforced polylactic acid (PLA) composite. Building direction, infill percentage, and layer height are the process variables consider...
Ausführliche Beschreibung
Autor*in: |
Kamaal, M. [verfasserIn] Anas, M. [verfasserIn] Rastogi, H. [verfasserIn] Bhardwaj, N. [verfasserIn] Rahaman, A. [verfasserIn] |
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Format: |
E-Artikel |
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Sprache: |
Englisch |
Erschienen: |
2020 |
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Schlagwörter: |
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Übergeordnetes Werk: |
Enthalten in: Progress in additive manufacturing - [Cham, Switzerland] : Springer International Publishing, 2016, 6(2020), 1 vom: 19. Aug., Seite 63-69 |
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Übergeordnetes Werk: |
volume:6 ; year:2020 ; number:1 ; day:19 ; month:08 ; pages:63-69 |
Links: |
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DOI / URN: |
10.1007/s40964-020-00145-3 |
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Katalog-ID: |
SPR043208320 |
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520 | |a Abstract This paper presents the effect of process parameters of the fused deposition modelling (FDM) method on mechanical properties of 3D-printed carbon fibre (CF)-reinforced polylactic acid (PLA) composite. Building direction, infill percentage, and layer height are the process variables considered for studies due to their high influencing factor in mechanical properties of product. Tensile strength and impact strength are the response parameters considered in the study. Multi-optimisation is done using TOPSIS (Technique for Order Preferences by Similarity to Ideal Solution) analysis to find the best set of parameters that would provide the maximum strength using minimum material. The material used is CF-reinforced PLA composite filament (1.75-mm diameter) for 3D printing. | ||
650 | 4 | |a Additive manufacturing |7 (dpeaa)DE-He213 | |
650 | 4 | |a Fused deposition modelling (FDM) |7 (dpeaa)DE-He213 | |
650 | 4 | |a Process parameters |7 (dpeaa)DE-He213 | |
650 | 4 | |a Mechanical properties |7 (dpeaa)DE-He213 | |
650 | 4 | |a TOPSIS |7 (dpeaa)DE-He213 | |
650 | 4 | |a Carbon fibre-reinforced PLA composite |7 (dpeaa)DE-He213 | |
700 | 1 | |a Anas, M. |e verfasserin |4 aut | |
700 | 1 | |a Rastogi, H. |e verfasserin |4 aut | |
700 | 1 | |a Bhardwaj, N. |e verfasserin |4 aut | |
700 | 1 | |a Rahaman, A. |e verfasserin |4 aut | |
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10.1007/s40964-020-00145-3 doi (DE-627)SPR043208320 (DE-599)SPRs40964-020-00145-3-e (SPR)s40964-020-00145-3-e DE-627 ger DE-627 rakwb eng 670 620 621.3 ASE 670 620 621.3 ASE 52.00 bkl Kamaal, M. verfasserin aut Effect of FDM process parameters on mechanical properties of 3D-printed carbon fibre–PLA composite 2020 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier Abstract This paper presents the effect of process parameters of the fused deposition modelling (FDM) method on mechanical properties of 3D-printed carbon fibre (CF)-reinforced polylactic acid (PLA) composite. Building direction, infill percentage, and layer height are the process variables considered for studies due to their high influencing factor in mechanical properties of product. Tensile strength and impact strength are the response parameters considered in the study. Multi-optimisation is done using TOPSIS (Technique for Order Preferences by Similarity to Ideal Solution) analysis to find the best set of parameters that would provide the maximum strength using minimum material. The material used is CF-reinforced PLA composite filament (1.75-mm diameter) for 3D printing. Additive manufacturing (dpeaa)DE-He213 Fused deposition modelling (FDM) (dpeaa)DE-He213 Process parameters (dpeaa)DE-He213 Mechanical properties (dpeaa)DE-He213 TOPSIS (dpeaa)DE-He213 Carbon fibre-reinforced PLA composite (dpeaa)DE-He213 Anas, M. verfasserin aut Rastogi, H. verfasserin aut Bhardwaj, N. verfasserin aut Rahaman, A. verfasserin aut Enthalten in Progress in additive manufacturing [Cham, Switzerland] : Springer International Publishing, 2016 6(2020), 1 vom: 19. Aug., Seite 63-69 (DE-627)843644087 (DE-600)2842521-2 2363-9520 nnns volume:6 year:2020 number:1 day:19 month:08 pages:63-69 https://dx.doi.org/10.1007/s40964-020-00145-3 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_266 GBV_ILN_281 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_636 GBV_ILN_702 GBV_ILN_2001 GBV_ILN_2003 GBV_ILN_2004 GBV_ILN_2005 GBV_ILN_2006 GBV_ILN_2007 GBV_ILN_2008 GBV_ILN_2009 GBV_ILN_2010 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_2025 GBV_ILN_2026 GBV_ILN_2027 GBV_ILN_2031 GBV_ILN_2034 GBV_ILN_2037 GBV_ILN_2038 GBV_ILN_2039 GBV_ILN_2044 GBV_ILN_2048 GBV_ILN_2049 GBV_ILN_2050 GBV_ILN_2055 GBV_ILN_2056 GBV_ILN_2057 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 GBV_ILN_2088 GBV_ILN_2093 GBV_ILN_2106 GBV_ILN_2107 GBV_ILN_2108 GBV_ILN_2110 GBV_ILN_2111 GBV_ILN_2112 GBV_ILN_2113 GBV_ILN_2118 GBV_ILN_2122 GBV_ILN_2129 GBV_ILN_2143 GBV_ILN_2144 GBV_ILN_2147 GBV_ILN_2148 GBV_ILN_2152 GBV_ILN_2153 GBV_ILN_2188 GBV_ILN_2190 GBV_ILN_2232 GBV_ILN_2336 GBV_ILN_2446 GBV_ILN_2470 GBV_ILN_2472 GBV_ILN_2507 GBV_ILN_2522 GBV_ILN_2548 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4046 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4242 GBV_ILN_4246 GBV_ILN_4249 GBV_ILN_4251 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4326 GBV_ILN_4328 GBV_ILN_4333 GBV_ILN_4334 GBV_ILN_4335 GBV_ILN_4336 GBV_ILN_4338 GBV_ILN_4393 GBV_ILN_4700 52.00 ASE AR 6 2020 1 19 08 63-69 |
spelling |
10.1007/s40964-020-00145-3 doi (DE-627)SPR043208320 (DE-599)SPRs40964-020-00145-3-e (SPR)s40964-020-00145-3-e DE-627 ger DE-627 rakwb eng 670 620 621.3 ASE 670 620 621.3 ASE 52.00 bkl Kamaal, M. verfasserin aut Effect of FDM process parameters on mechanical properties of 3D-printed carbon fibre–PLA composite 2020 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier Abstract This paper presents the effect of process parameters of the fused deposition modelling (FDM) method on mechanical properties of 3D-printed carbon fibre (CF)-reinforced polylactic acid (PLA) composite. Building direction, infill percentage, and layer height are the process variables considered for studies due to their high influencing factor in mechanical properties of product. Tensile strength and impact strength are the response parameters considered in the study. Multi-optimisation is done using TOPSIS (Technique for Order Preferences by Similarity to Ideal Solution) analysis to find the best set of parameters that would provide the maximum strength using minimum material. The material used is CF-reinforced PLA composite filament (1.75-mm diameter) for 3D printing. Additive manufacturing (dpeaa)DE-He213 Fused deposition modelling (FDM) (dpeaa)DE-He213 Process parameters (dpeaa)DE-He213 Mechanical properties (dpeaa)DE-He213 TOPSIS (dpeaa)DE-He213 Carbon fibre-reinforced PLA composite (dpeaa)DE-He213 Anas, M. verfasserin aut Rastogi, H. verfasserin aut Bhardwaj, N. verfasserin aut Rahaman, A. verfasserin aut Enthalten in Progress in additive manufacturing [Cham, Switzerland] : Springer International Publishing, 2016 6(2020), 1 vom: 19. Aug., Seite 63-69 (DE-627)843644087 (DE-600)2842521-2 2363-9520 nnns volume:6 year:2020 number:1 day:19 month:08 pages:63-69 https://dx.doi.org/10.1007/s40964-020-00145-3 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_266 GBV_ILN_281 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_636 GBV_ILN_702 GBV_ILN_2001 GBV_ILN_2003 GBV_ILN_2004 GBV_ILN_2005 GBV_ILN_2006 GBV_ILN_2007 GBV_ILN_2008 GBV_ILN_2009 GBV_ILN_2010 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_2025 GBV_ILN_2026 GBV_ILN_2027 GBV_ILN_2031 GBV_ILN_2034 GBV_ILN_2037 GBV_ILN_2038 GBV_ILN_2039 GBV_ILN_2044 GBV_ILN_2048 GBV_ILN_2049 GBV_ILN_2050 GBV_ILN_2055 GBV_ILN_2056 GBV_ILN_2057 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 GBV_ILN_2088 GBV_ILN_2093 GBV_ILN_2106 GBV_ILN_2107 GBV_ILN_2108 GBV_ILN_2110 GBV_ILN_2111 GBV_ILN_2112 GBV_ILN_2113 GBV_ILN_2118 GBV_ILN_2122 GBV_ILN_2129 GBV_ILN_2143 GBV_ILN_2144 GBV_ILN_2147 GBV_ILN_2148 GBV_ILN_2152 GBV_ILN_2153 GBV_ILN_2188 GBV_ILN_2190 GBV_ILN_2232 GBV_ILN_2336 GBV_ILN_2446 GBV_ILN_2470 GBV_ILN_2472 GBV_ILN_2507 GBV_ILN_2522 GBV_ILN_2548 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4046 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4242 GBV_ILN_4246 GBV_ILN_4249 GBV_ILN_4251 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4326 GBV_ILN_4328 GBV_ILN_4333 GBV_ILN_4334 GBV_ILN_4335 GBV_ILN_4336 GBV_ILN_4338 GBV_ILN_4393 GBV_ILN_4700 52.00 ASE AR 6 2020 1 19 08 63-69 |
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10.1007/s40964-020-00145-3 doi (DE-627)SPR043208320 (DE-599)SPRs40964-020-00145-3-e (SPR)s40964-020-00145-3-e DE-627 ger DE-627 rakwb eng 670 620 621.3 ASE 670 620 621.3 ASE 52.00 bkl Kamaal, M. verfasserin aut Effect of FDM process parameters on mechanical properties of 3D-printed carbon fibre–PLA composite 2020 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier Abstract This paper presents the effect of process parameters of the fused deposition modelling (FDM) method on mechanical properties of 3D-printed carbon fibre (CF)-reinforced polylactic acid (PLA) composite. Building direction, infill percentage, and layer height are the process variables considered for studies due to their high influencing factor in mechanical properties of product. Tensile strength and impact strength are the response parameters considered in the study. Multi-optimisation is done using TOPSIS (Technique for Order Preferences by Similarity to Ideal Solution) analysis to find the best set of parameters that would provide the maximum strength using minimum material. The material used is CF-reinforced PLA composite filament (1.75-mm diameter) for 3D printing. Additive manufacturing (dpeaa)DE-He213 Fused deposition modelling (FDM) (dpeaa)DE-He213 Process parameters (dpeaa)DE-He213 Mechanical properties (dpeaa)DE-He213 TOPSIS (dpeaa)DE-He213 Carbon fibre-reinforced PLA composite (dpeaa)DE-He213 Anas, M. verfasserin aut Rastogi, H. verfasserin aut Bhardwaj, N. verfasserin aut Rahaman, A. verfasserin aut Enthalten in Progress in additive manufacturing [Cham, Switzerland] : Springer International Publishing, 2016 6(2020), 1 vom: 19. Aug., Seite 63-69 (DE-627)843644087 (DE-600)2842521-2 2363-9520 nnns volume:6 year:2020 number:1 day:19 month:08 pages:63-69 https://dx.doi.org/10.1007/s40964-020-00145-3 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_266 GBV_ILN_281 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_636 GBV_ILN_702 GBV_ILN_2001 GBV_ILN_2003 GBV_ILN_2004 GBV_ILN_2005 GBV_ILN_2006 GBV_ILN_2007 GBV_ILN_2008 GBV_ILN_2009 GBV_ILN_2010 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_2025 GBV_ILN_2026 GBV_ILN_2027 GBV_ILN_2031 GBV_ILN_2034 GBV_ILN_2037 GBV_ILN_2038 GBV_ILN_2039 GBV_ILN_2044 GBV_ILN_2048 GBV_ILN_2049 GBV_ILN_2050 GBV_ILN_2055 GBV_ILN_2056 GBV_ILN_2057 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 GBV_ILN_2088 GBV_ILN_2093 GBV_ILN_2106 GBV_ILN_2107 GBV_ILN_2108 GBV_ILN_2110 GBV_ILN_2111 GBV_ILN_2112 GBV_ILN_2113 GBV_ILN_2118 GBV_ILN_2122 GBV_ILN_2129 GBV_ILN_2143 GBV_ILN_2144 GBV_ILN_2147 GBV_ILN_2148 GBV_ILN_2152 GBV_ILN_2153 GBV_ILN_2188 GBV_ILN_2190 GBV_ILN_2232 GBV_ILN_2336 GBV_ILN_2446 GBV_ILN_2470 GBV_ILN_2472 GBV_ILN_2507 GBV_ILN_2522 GBV_ILN_2548 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4046 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4242 GBV_ILN_4246 GBV_ILN_4249 GBV_ILN_4251 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4326 GBV_ILN_4328 GBV_ILN_4333 GBV_ILN_4334 GBV_ILN_4335 GBV_ILN_4336 GBV_ILN_4338 GBV_ILN_4393 GBV_ILN_4700 52.00 ASE AR 6 2020 1 19 08 63-69 |
allfieldsGer |
10.1007/s40964-020-00145-3 doi (DE-627)SPR043208320 (DE-599)SPRs40964-020-00145-3-e (SPR)s40964-020-00145-3-e DE-627 ger DE-627 rakwb eng 670 620 621.3 ASE 670 620 621.3 ASE 52.00 bkl Kamaal, M. verfasserin aut Effect of FDM process parameters on mechanical properties of 3D-printed carbon fibre–PLA composite 2020 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier Abstract This paper presents the effect of process parameters of the fused deposition modelling (FDM) method on mechanical properties of 3D-printed carbon fibre (CF)-reinforced polylactic acid (PLA) composite. Building direction, infill percentage, and layer height are the process variables considered for studies due to their high influencing factor in mechanical properties of product. Tensile strength and impact strength are the response parameters considered in the study. Multi-optimisation is done using TOPSIS (Technique for Order Preferences by Similarity to Ideal Solution) analysis to find the best set of parameters that would provide the maximum strength using minimum material. The material used is CF-reinforced PLA composite filament (1.75-mm diameter) for 3D printing. Additive manufacturing (dpeaa)DE-He213 Fused deposition modelling (FDM) (dpeaa)DE-He213 Process parameters (dpeaa)DE-He213 Mechanical properties (dpeaa)DE-He213 TOPSIS (dpeaa)DE-He213 Carbon fibre-reinforced PLA composite (dpeaa)DE-He213 Anas, M. verfasserin aut Rastogi, H. verfasserin aut Bhardwaj, N. verfasserin aut Rahaman, A. verfasserin aut Enthalten in Progress in additive manufacturing [Cham, Switzerland] : Springer International Publishing, 2016 6(2020), 1 vom: 19. Aug., Seite 63-69 (DE-627)843644087 (DE-600)2842521-2 2363-9520 nnns volume:6 year:2020 number:1 day:19 month:08 pages:63-69 https://dx.doi.org/10.1007/s40964-020-00145-3 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_266 GBV_ILN_281 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_636 GBV_ILN_702 GBV_ILN_2001 GBV_ILN_2003 GBV_ILN_2004 GBV_ILN_2005 GBV_ILN_2006 GBV_ILN_2007 GBV_ILN_2008 GBV_ILN_2009 GBV_ILN_2010 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_2025 GBV_ILN_2026 GBV_ILN_2027 GBV_ILN_2031 GBV_ILN_2034 GBV_ILN_2037 GBV_ILN_2038 GBV_ILN_2039 GBV_ILN_2044 GBV_ILN_2048 GBV_ILN_2049 GBV_ILN_2050 GBV_ILN_2055 GBV_ILN_2056 GBV_ILN_2057 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 GBV_ILN_2088 GBV_ILN_2093 GBV_ILN_2106 GBV_ILN_2107 GBV_ILN_2108 GBV_ILN_2110 GBV_ILN_2111 GBV_ILN_2112 GBV_ILN_2113 GBV_ILN_2118 GBV_ILN_2122 GBV_ILN_2129 GBV_ILN_2143 GBV_ILN_2144 GBV_ILN_2147 GBV_ILN_2148 GBV_ILN_2152 GBV_ILN_2153 GBV_ILN_2188 GBV_ILN_2190 GBV_ILN_2232 GBV_ILN_2336 GBV_ILN_2446 GBV_ILN_2470 GBV_ILN_2472 GBV_ILN_2507 GBV_ILN_2522 GBV_ILN_2548 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4046 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4242 GBV_ILN_4246 GBV_ILN_4249 GBV_ILN_4251 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4326 GBV_ILN_4328 GBV_ILN_4333 GBV_ILN_4334 GBV_ILN_4335 GBV_ILN_4336 GBV_ILN_4338 GBV_ILN_4393 GBV_ILN_4700 52.00 ASE AR 6 2020 1 19 08 63-69 |
allfieldsSound |
10.1007/s40964-020-00145-3 doi (DE-627)SPR043208320 (DE-599)SPRs40964-020-00145-3-e (SPR)s40964-020-00145-3-e DE-627 ger DE-627 rakwb eng 670 620 621.3 ASE 670 620 621.3 ASE 52.00 bkl Kamaal, M. verfasserin aut Effect of FDM process parameters on mechanical properties of 3D-printed carbon fibre–PLA composite 2020 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier Abstract This paper presents the effect of process parameters of the fused deposition modelling (FDM) method on mechanical properties of 3D-printed carbon fibre (CF)-reinforced polylactic acid (PLA) composite. Building direction, infill percentage, and layer height are the process variables considered for studies due to their high influencing factor in mechanical properties of product. Tensile strength and impact strength are the response parameters considered in the study. Multi-optimisation is done using TOPSIS (Technique for Order Preferences by Similarity to Ideal Solution) analysis to find the best set of parameters that would provide the maximum strength using minimum material. The material used is CF-reinforced PLA composite filament (1.75-mm diameter) for 3D printing. Additive manufacturing (dpeaa)DE-He213 Fused deposition modelling (FDM) (dpeaa)DE-He213 Process parameters (dpeaa)DE-He213 Mechanical properties (dpeaa)DE-He213 TOPSIS (dpeaa)DE-He213 Carbon fibre-reinforced PLA composite (dpeaa)DE-He213 Anas, M. verfasserin aut Rastogi, H. verfasserin aut Bhardwaj, N. verfasserin aut Rahaman, A. verfasserin aut Enthalten in Progress in additive manufacturing [Cham, Switzerland] : Springer International Publishing, 2016 6(2020), 1 vom: 19. Aug., Seite 63-69 (DE-627)843644087 (DE-600)2842521-2 2363-9520 nnns volume:6 year:2020 number:1 day:19 month:08 pages:63-69 https://dx.doi.org/10.1007/s40964-020-00145-3 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_266 GBV_ILN_281 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_636 GBV_ILN_702 GBV_ILN_2001 GBV_ILN_2003 GBV_ILN_2004 GBV_ILN_2005 GBV_ILN_2006 GBV_ILN_2007 GBV_ILN_2008 GBV_ILN_2009 GBV_ILN_2010 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_2025 GBV_ILN_2026 GBV_ILN_2027 GBV_ILN_2031 GBV_ILN_2034 GBV_ILN_2037 GBV_ILN_2038 GBV_ILN_2039 GBV_ILN_2044 GBV_ILN_2048 GBV_ILN_2049 GBV_ILN_2050 GBV_ILN_2055 GBV_ILN_2056 GBV_ILN_2057 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 GBV_ILN_2088 GBV_ILN_2093 GBV_ILN_2106 GBV_ILN_2107 GBV_ILN_2108 GBV_ILN_2110 GBV_ILN_2111 GBV_ILN_2112 GBV_ILN_2113 GBV_ILN_2118 GBV_ILN_2122 GBV_ILN_2129 GBV_ILN_2143 GBV_ILN_2144 GBV_ILN_2147 GBV_ILN_2148 GBV_ILN_2152 GBV_ILN_2153 GBV_ILN_2188 GBV_ILN_2190 GBV_ILN_2232 GBV_ILN_2336 GBV_ILN_2446 GBV_ILN_2470 GBV_ILN_2472 GBV_ILN_2507 GBV_ILN_2522 GBV_ILN_2548 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4046 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4242 GBV_ILN_4246 GBV_ILN_4249 GBV_ILN_4251 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4326 GBV_ILN_4328 GBV_ILN_4333 GBV_ILN_4334 GBV_ILN_4335 GBV_ILN_4336 GBV_ILN_4338 GBV_ILN_4393 GBV_ILN_4700 52.00 ASE AR 6 2020 1 19 08 63-69 |
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Enthalten in Progress in additive manufacturing 6(2020), 1 vom: 19. Aug., Seite 63-69 volume:6 year:2020 number:1 day:19 month:08 pages:63-69 |
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Kamaal, M. @@aut@@ Anas, M. @@aut@@ Rastogi, H. @@aut@@ Bhardwaj, N. @@aut@@ Rahaman, A. @@aut@@ |
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<?xml version="1.0" encoding="UTF-8"?><collection xmlns="http://www.loc.gov/MARC21/slim"><record><leader>01000caa a22002652 4500</leader><controlfield tag="001">SPR043208320</controlfield><controlfield tag="003">DE-627</controlfield><controlfield tag="005">20220112034911.0</controlfield><controlfield tag="007">cr uuu---uuuuu</controlfield><controlfield tag="008">210217s2020 xx |||||o 00| ||eng c</controlfield><datafield tag="024" ind1="7" ind2=" "><subfield code="a">10.1007/s40964-020-00145-3</subfield><subfield code="2">doi</subfield></datafield><datafield tag="035" ind1=" " ind2=" "><subfield code="a">(DE-627)SPR043208320</subfield></datafield><datafield tag="035" ind1=" " ind2=" "><subfield code="a">(DE-599)SPRs40964-020-00145-3-e</subfield></datafield><datafield tag="035" ind1=" " ind2=" "><subfield code="a">(SPR)s40964-020-00145-3-e</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="a">620</subfield><subfield code="a">621.3</subfield><subfield code="q">ASE</subfield></datafield><datafield tag="082" ind1="0" ind2="4"><subfield code="a">670</subfield><subfield code="a">620</subfield><subfield code="a">621.3</subfield><subfield code="q">ASE</subfield></datafield><datafield tag="084" ind1=" " ind2=" "><subfield code="a">52.00</subfield><subfield code="2">bkl</subfield></datafield><datafield tag="100" ind1="1" ind2=" "><subfield code="a">Kamaal, M.</subfield><subfield code="e">verfasserin</subfield><subfield code="4">aut</subfield></datafield><datafield tag="245" ind1="1" ind2="0"><subfield code="a">Effect of FDM process parameters on mechanical properties of 3D-printed carbon fibre–PLA composite</subfield></datafield><datafield tag="264" ind1=" " ind2="1"><subfield code="c">2020</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="520" ind1=" " ind2=" "><subfield code="a">Abstract This paper presents the effect of process parameters of the fused deposition modelling (FDM) method on mechanical properties of 3D-printed carbon fibre (CF)-reinforced polylactic acid (PLA) composite. Building direction, infill percentage, and layer height are the process variables considered for studies due to their high influencing factor in mechanical properties of product. Tensile strength and impact strength are the response parameters considered in the study. Multi-optimisation is done using TOPSIS (Technique for Order Preferences by Similarity to Ideal Solution) analysis to find the best set of parameters that would provide the maximum strength using minimum material. 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Kamaal, M. |
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Kamaal, M. ddc 670 bkl 52.00 misc Additive manufacturing misc Fused deposition modelling (FDM) misc Process parameters misc Mechanical properties misc TOPSIS misc Carbon fibre-reinforced PLA composite Effect of FDM process parameters on mechanical properties of 3D-printed carbon fibre–PLA composite |
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670 620 621.3 ASE 52.00 bkl Effect of FDM process parameters on mechanical properties of 3D-printed carbon fibre–PLA composite Additive manufacturing (dpeaa)DE-He213 Fused deposition modelling (FDM) (dpeaa)DE-He213 Process parameters (dpeaa)DE-He213 Mechanical properties (dpeaa)DE-He213 TOPSIS (dpeaa)DE-He213 Carbon fibre-reinforced PLA composite (dpeaa)DE-He213 |
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ddc 670 bkl 52.00 misc Additive manufacturing misc Fused deposition modelling (FDM) misc Process parameters misc Mechanical properties misc TOPSIS misc Carbon fibre-reinforced PLA composite |
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ddc 670 bkl 52.00 misc Additive manufacturing misc Fused deposition modelling (FDM) misc Process parameters misc Mechanical properties misc TOPSIS misc Carbon fibre-reinforced PLA composite |
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Effect of FDM process parameters on mechanical properties of 3D-printed carbon fibre–PLA composite |
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Effect of FDM process parameters on mechanical properties of 3D-printed carbon fibre–PLA composite |
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effect of fdm process parameters on mechanical properties of 3d-printed carbon fibre–pla composite |
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Effect of FDM process parameters on mechanical properties of 3D-printed carbon fibre–PLA composite |
abstract |
Abstract This paper presents the effect of process parameters of the fused deposition modelling (FDM) method on mechanical properties of 3D-printed carbon fibre (CF)-reinforced polylactic acid (PLA) composite. Building direction, infill percentage, and layer height are the process variables considered for studies due to their high influencing factor in mechanical properties of product. Tensile strength and impact strength are the response parameters considered in the study. Multi-optimisation is done using TOPSIS (Technique for Order Preferences by Similarity to Ideal Solution) analysis to find the best set of parameters that would provide the maximum strength using minimum material. The material used is CF-reinforced PLA composite filament (1.75-mm diameter) for 3D printing. |
abstractGer |
Abstract This paper presents the effect of process parameters of the fused deposition modelling (FDM) method on mechanical properties of 3D-printed carbon fibre (CF)-reinforced polylactic acid (PLA) composite. Building direction, infill percentage, and layer height are the process variables considered for studies due to their high influencing factor in mechanical properties of product. Tensile strength and impact strength are the response parameters considered in the study. Multi-optimisation is done using TOPSIS (Technique for Order Preferences by Similarity to Ideal Solution) analysis to find the best set of parameters that would provide the maximum strength using minimum material. The material used is CF-reinforced PLA composite filament (1.75-mm diameter) for 3D printing. |
abstract_unstemmed |
Abstract This paper presents the effect of process parameters of the fused deposition modelling (FDM) method on mechanical properties of 3D-printed carbon fibre (CF)-reinforced polylactic acid (PLA) composite. Building direction, infill percentage, and layer height are the process variables considered for studies due to their high influencing factor in mechanical properties of product. Tensile strength and impact strength are the response parameters considered in the study. Multi-optimisation is done using TOPSIS (Technique for Order Preferences by Similarity to Ideal Solution) analysis to find the best set of parameters that would provide the maximum strength using minimum material. The material used is CF-reinforced PLA composite filament (1.75-mm diameter) for 3D printing. |
collection_details |
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container_issue |
1 |
title_short |
Effect of FDM process parameters on mechanical properties of 3D-printed carbon fibre–PLA composite |
url |
https://dx.doi.org/10.1007/s40964-020-00145-3 |
remote_bool |
true |
author2 |
Anas, M. Rastogi, H. Bhardwaj, N. Rahaman, A. |
author2Str |
Anas, M. Rastogi, H. Bhardwaj, N. Rahaman, A. |
ppnlink |
843644087 |
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hochschulschrift_bool |
false |
doi_str |
10.1007/s40964-020-00145-3 |
up_date |
2024-07-03T17:14:44.958Z |
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score |
7.3988237 |