Through-thickness heterogeneity and in-plane anisotropy in creep aging of 7050 Al alloy

During creep aging (CA), through-thickness heterogeneity and in-plane anisotropy in creep and mechanical properties affect the shape forming and performance tailoring. The specimens are first machined from the surface (t1), subsurface (t2) and center (t3) layers along the thickness direction of the...
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Autor*in:	T.J. Bian [verfasserIn] H. Li [verfasserIn] J.C. Yang [verfasserIn] C. Lei [verfasserIn] C.H. Wu [verfasserIn] L.W. Zhang [verfasserIn] G.Y. Chen [verfasserIn]

Format:	E-Artikel
Sprache:	Englisch

Erschienen:	2020

Schlagwörter:	Creep aging Through-thickness heterogeneity In-plane anisotropy Low angle grain boundary Texture 7050 Al alloy

Übergeordnetes Werk:	In: Materials & Design - Elsevier, 2019, 196(2020), Seite 109190-
Übergeordnetes Werk:	volume:196 ; year:2020 ; pages:109190-

Links:	Link aufrufen Link aufrufen Link aufrufen Journal toc

DOI / URN:	10.1016/j.matdes.2020.109190

Katalog-ID:	DOAJ007037031

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520			\|a During creep aging (CA), through-thickness heterogeneity and in-plane anisotropy in creep and mechanical properties affect the shape forming and performance tailoring. The specimens are first machined from the surface (t1), subsurface (t2) and center (t3) layers along the thickness direction of the 7050 Al alloy plate. Then in the rolling plane of each layer, the specimens are taken along the angles of 0° (L0), 45° (L45) and 90° (L90) to the rolling direction. After CA, the creep strain shows the trends of t1 < t2 < t3 along the thickness direction and L45 < L90 < L0 for in-plane directions, while the yield strength (YS) shows t1 < t3 < t2 and L90 < L0 < L45, respectively.Before CA, the low-angle grain boundaries (LAGBs) increase along the thickness direction, leading to a reduced creep strain. After CA, through-thickness heterogeneous LAGBs contributes to the above trend of YS. After L45 and L90 loading, S, Brass and Copper textures are obviously weaker than that under L0 loading, and show the largest equivalent Schmid factor (ESF) for L45 loading, and that for L0 and L90 conditions are approaching; while the equivalent slip system number (ESSN) shows L90 < L0 < L45. Both ESF and ESSN determine the in-plane anisotropy by affecting dislocation slip, but ESF plays a dominant role.
650		4	\|a Creep aging
650		4	\|a Through-thickness heterogeneity
650		4	\|a In-plane anisotropy
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650		4	\|a 7050 Al alloy
653		0	\|a Materials of engineering and construction. Mechanics of materials
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700	0		\|a L.W. Zhang \|e verfasserin \|4 aut
700	0		\|a G.Y. Chen \|e verfasserin \|4 aut
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allfields	10.1016/j.matdes.2020.109190 doi (DE-627)DOAJ007037031 (DE-599)DOAJ5717b7e46e5e46a5b79cf74557409818 DE-627 ger DE-627 rakwb eng TA401-492 T.J. Bian verfasserin aut Through-thickness heterogeneity and in-plane anisotropy in creep aging of 7050 Al alloy 2020 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier During creep aging (CA), through-thickness heterogeneity and in-plane anisotropy in creep and mechanical properties affect the shape forming and performance tailoring. The specimens are first machined from the surface (t1), subsurface (t2) and center (t3) layers along the thickness direction of the 7050 Al alloy plate. Then in the rolling plane of each layer, the specimens are taken along the angles of 0° (L0), 45° (L45) and 90° (L90) to the rolling direction. After CA, the creep strain shows the trends of t1 < t2 < t3 along the thickness direction and L45 < L90 < L0 for in-plane directions, while the yield strength (YS) shows t1 < t3 < t2 and L90 < L0 < L45, respectively.Before CA, the low-angle grain boundaries (LAGBs) increase along the thickness direction, leading to a reduced creep strain. After CA, through-thickness heterogeneous LAGBs contributes to the above trend of YS. After L45 and L90 loading, S, Brass and Copper textures are obviously weaker than that under L0 loading, and show the largest equivalent Schmid factor (ESF) for L45 loading, and that for L0 and L90 conditions are approaching; while the equivalent slip system number (ESSN) shows L90 < L0 < L45. Both ESF and ESSN determine the in-plane anisotropy by affecting dislocation slip, but ESF plays a dominant role. Creep aging Through-thickness heterogeneity In-plane anisotropy Low angle grain boundary Texture 7050 Al alloy Materials of engineering and construction. Mechanics of materials H. Li verfasserin aut J.C. Yang verfasserin aut C. Lei verfasserin aut C.H. Wu verfasserin aut L.W. Zhang verfasserin aut G.Y. Chen verfasserin aut In Materials & Design Elsevier, 2019 196(2020), Seite 109190- (DE-627)32052857X (DE-600)2015480-X 18734197 nnns volume:196 year:2020 pages:109190- https://doi.org/10.1016/j.matdes.2020.109190 kostenfrei https://doaj.org/article/5717b7e46e5e46a5b79cf74557409818 kostenfrei http://www.sciencedirect.com/science/article/pii/S0264127520307255 kostenfrei https://doaj.org/toc/0264-1275 Journal toc kostenfrei GBV_USEFLAG_A SYSFLAG_A GBV_DOAJ SSG-OLC-PHA GBV_ILN_11 GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 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_95 GBV_ILN_105 GBV_ILN_110 GBV_ILN_150 GBV_ILN_151 GBV_ILN_161 GBV_ILN_165 GBV_ILN_170 GBV_ILN_213 GBV_ILN_224 GBV_ILN_230 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_2001 GBV_ILN_2003 GBV_ILN_2004 GBV_ILN_2005 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_2038 GBV_ILN_2044 GBV_ILN_2048 GBV_ILN_2049 GBV_ILN_2050 GBV_ILN_2055 GBV_ILN_2056 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 GBV_ILN_2088 GBV_ILN_2106 GBV_ILN_2110 GBV_ILN_2111 GBV_ILN_2112 GBV_ILN_2118 GBV_ILN_2122 GBV_ILN_2129 GBV_ILN_2143 GBV_ILN_2147 GBV_ILN_2148 GBV_ILN_2152 GBV_ILN_2153 GBV_ILN_2190 GBV_ILN_2232 GBV_ILN_2336 GBV_ILN_2470 GBV_ILN_2472 GBV_ILN_2507 GBV_ILN_2548 GBV_ILN_4012 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4046 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4242 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_4338 GBV_ILN_4367 GBV_ILN_4393 GBV_ILN_4700 AR 196 2020 109190-
spelling	10.1016/j.matdes.2020.109190 doi (DE-627)DOAJ007037031 (DE-599)DOAJ5717b7e46e5e46a5b79cf74557409818 DE-627 ger DE-627 rakwb eng TA401-492 T.J. Bian verfasserin aut Through-thickness heterogeneity and in-plane anisotropy in creep aging of 7050 Al alloy 2020 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier During creep aging (CA), through-thickness heterogeneity and in-plane anisotropy in creep and mechanical properties affect the shape forming and performance tailoring. The specimens are first machined from the surface (t1), subsurface (t2) and center (t3) layers along the thickness direction of the 7050 Al alloy plate. Then in the rolling plane of each layer, the specimens are taken along the angles of 0° (L0), 45° (L45) and 90° (L90) to the rolling direction. After CA, the creep strain shows the trends of t1 < t2 < t3 along the thickness direction and L45 < L90 < L0 for in-plane directions, while the yield strength (YS) shows t1 < t3 < t2 and L90 < L0 < L45, respectively.Before CA, the low-angle grain boundaries (LAGBs) increase along the thickness direction, leading to a reduced creep strain. After CA, through-thickness heterogeneous LAGBs contributes to the above trend of YS. After L45 and L90 loading, S, Brass and Copper textures are obviously weaker than that under L0 loading, and show the largest equivalent Schmid factor (ESF) for L45 loading, and that for L0 and L90 conditions are approaching; while the equivalent slip system number (ESSN) shows L90 < L0 < L45. Both ESF and ESSN determine the in-plane anisotropy by affecting dislocation slip, but ESF plays a dominant role. Creep aging Through-thickness heterogeneity In-plane anisotropy Low angle grain boundary Texture 7050 Al alloy Materials of engineering and construction. Mechanics of materials H. Li verfasserin aut J.C. Yang verfasserin aut C. Lei verfasserin aut C.H. Wu verfasserin aut L.W. Zhang verfasserin aut G.Y. Chen verfasserin aut In Materials & Design Elsevier, 2019 196(2020), Seite 109190- (DE-627)32052857X (DE-600)2015480-X 18734197 nnns volume:196 year:2020 pages:109190- https://doi.org/10.1016/j.matdes.2020.109190 kostenfrei https://doaj.org/article/5717b7e46e5e46a5b79cf74557409818 kostenfrei http://www.sciencedirect.com/science/article/pii/S0264127520307255 kostenfrei https://doaj.org/toc/0264-1275 Journal toc kostenfrei GBV_USEFLAG_A SYSFLAG_A GBV_DOAJ SSG-OLC-PHA GBV_ILN_11 GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 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_95 GBV_ILN_105 GBV_ILN_110 GBV_ILN_150 GBV_ILN_151 GBV_ILN_161 GBV_ILN_165 GBV_ILN_170 GBV_ILN_213 GBV_ILN_224 GBV_ILN_230 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_2001 GBV_ILN_2003 GBV_ILN_2004 GBV_ILN_2005 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_2038 GBV_ILN_2044 GBV_ILN_2048 GBV_ILN_2049 GBV_ILN_2050 GBV_ILN_2055 GBV_ILN_2056 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 GBV_ILN_2088 GBV_ILN_2106 GBV_ILN_2110 GBV_ILN_2111 GBV_ILN_2112 GBV_ILN_2118 GBV_ILN_2122 GBV_ILN_2129 GBV_ILN_2143 GBV_ILN_2147 GBV_ILN_2148 GBV_ILN_2152 GBV_ILN_2153 GBV_ILN_2190 GBV_ILN_2232 GBV_ILN_2336 GBV_ILN_2470 GBV_ILN_2472 GBV_ILN_2507 GBV_ILN_2548 GBV_ILN_4012 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4046 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4242 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_4338 GBV_ILN_4367 GBV_ILN_4393 GBV_ILN_4700 AR 196 2020 109190-
allfields_unstemmed	10.1016/j.matdes.2020.109190 doi (DE-627)DOAJ007037031 (DE-599)DOAJ5717b7e46e5e46a5b79cf74557409818 DE-627 ger DE-627 rakwb eng TA401-492 T.J. Bian verfasserin aut Through-thickness heterogeneity and in-plane anisotropy in creep aging of 7050 Al alloy 2020 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier During creep aging (CA), through-thickness heterogeneity and in-plane anisotropy in creep and mechanical properties affect the shape forming and performance tailoring. The specimens are first machined from the surface (t1), subsurface (t2) and center (t3) layers along the thickness direction of the 7050 Al alloy plate. Then in the rolling plane of each layer, the specimens are taken along the angles of 0° (L0), 45° (L45) and 90° (L90) to the rolling direction. After CA, the creep strain shows the trends of t1 < t2 < t3 along the thickness direction and L45 < L90 < L0 for in-plane directions, while the yield strength (YS) shows t1 < t3 < t2 and L90 < L0 < L45, respectively.Before CA, the low-angle grain boundaries (LAGBs) increase along the thickness direction, leading to a reduced creep strain. After CA, through-thickness heterogeneous LAGBs contributes to the above trend of YS. After L45 and L90 loading, S, Brass and Copper textures are obviously weaker than that under L0 loading, and show the largest equivalent Schmid factor (ESF) for L45 loading, and that for L0 and L90 conditions are approaching; while the equivalent slip system number (ESSN) shows L90 < L0 < L45. Both ESF and ESSN determine the in-plane anisotropy by affecting dislocation slip, but ESF plays a dominant role. Creep aging Through-thickness heterogeneity In-plane anisotropy Low angle grain boundary Texture 7050 Al alloy Materials of engineering and construction. Mechanics of materials H. Li verfasserin aut J.C. Yang verfasserin aut C. Lei verfasserin aut C.H. Wu verfasserin aut L.W. Zhang verfasserin aut G.Y. Chen verfasserin aut In Materials & Design Elsevier, 2019 196(2020), Seite 109190- (DE-627)32052857X (DE-600)2015480-X 18734197 nnns volume:196 year:2020 pages:109190- https://doi.org/10.1016/j.matdes.2020.109190 kostenfrei https://doaj.org/article/5717b7e46e5e46a5b79cf74557409818 kostenfrei http://www.sciencedirect.com/science/article/pii/S0264127520307255 kostenfrei https://doaj.org/toc/0264-1275 Journal toc kostenfrei GBV_USEFLAG_A SYSFLAG_A GBV_DOAJ SSG-OLC-PHA GBV_ILN_11 GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 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_95 GBV_ILN_105 GBV_ILN_110 GBV_ILN_150 GBV_ILN_151 GBV_ILN_161 GBV_ILN_165 GBV_ILN_170 GBV_ILN_213 GBV_ILN_224 GBV_ILN_230 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_2001 GBV_ILN_2003 GBV_ILN_2004 GBV_ILN_2005 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_2038 GBV_ILN_2044 GBV_ILN_2048 GBV_ILN_2049 GBV_ILN_2050 GBV_ILN_2055 GBV_ILN_2056 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 GBV_ILN_2088 GBV_ILN_2106 GBV_ILN_2110 GBV_ILN_2111 GBV_ILN_2112 GBV_ILN_2118 GBV_ILN_2122 GBV_ILN_2129 GBV_ILN_2143 GBV_ILN_2147 GBV_ILN_2148 GBV_ILN_2152 GBV_ILN_2153 GBV_ILN_2190 GBV_ILN_2232 GBV_ILN_2336 GBV_ILN_2470 GBV_ILN_2472 GBV_ILN_2507 GBV_ILN_2548 GBV_ILN_4012 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4046 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4242 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_4338 GBV_ILN_4367 GBV_ILN_4393 GBV_ILN_4700 AR 196 2020 109190-
allfieldsGer	10.1016/j.matdes.2020.109190 doi (DE-627)DOAJ007037031 (DE-599)DOAJ5717b7e46e5e46a5b79cf74557409818 DE-627 ger DE-627 rakwb eng TA401-492 T.J. Bian verfasserin aut Through-thickness heterogeneity and in-plane anisotropy in creep aging of 7050 Al alloy 2020 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier During creep aging (CA), through-thickness heterogeneity and in-plane anisotropy in creep and mechanical properties affect the shape forming and performance tailoring. The specimens are first machined from the surface (t1), subsurface (t2) and center (t3) layers along the thickness direction of the 7050 Al alloy plate. Then in the rolling plane of each layer, the specimens are taken along the angles of 0° (L0), 45° (L45) and 90° (L90) to the rolling direction. After CA, the creep strain shows the trends of t1 < t2 < t3 along the thickness direction and L45 < L90 < L0 for in-plane directions, while the yield strength (YS) shows t1 < t3 < t2 and L90 < L0 < L45, respectively.Before CA, the low-angle grain boundaries (LAGBs) increase along the thickness direction, leading to a reduced creep strain. After CA, through-thickness heterogeneous LAGBs contributes to the above trend of YS. After L45 and L90 loading, S, Brass and Copper textures are obviously weaker than that under L0 loading, and show the largest equivalent Schmid factor (ESF) for L45 loading, and that for L0 and L90 conditions are approaching; while the equivalent slip system number (ESSN) shows L90 < L0 < L45. Both ESF and ESSN determine the in-plane anisotropy by affecting dislocation slip, but ESF plays a dominant role. Creep aging Through-thickness heterogeneity In-plane anisotropy Low angle grain boundary Texture 7050 Al alloy Materials of engineering and construction. Mechanics of materials H. Li verfasserin aut J.C. Yang verfasserin aut C. Lei verfasserin aut C.H. Wu verfasserin aut L.W. Zhang verfasserin aut G.Y. Chen verfasserin aut In Materials & Design Elsevier, 2019 196(2020), Seite 109190- (DE-627)32052857X (DE-600)2015480-X 18734197 nnns volume:196 year:2020 pages:109190- https://doi.org/10.1016/j.matdes.2020.109190 kostenfrei https://doaj.org/article/5717b7e46e5e46a5b79cf74557409818 kostenfrei http://www.sciencedirect.com/science/article/pii/S0264127520307255 kostenfrei https://doaj.org/toc/0264-1275 Journal toc kostenfrei GBV_USEFLAG_A SYSFLAG_A GBV_DOAJ SSG-OLC-PHA GBV_ILN_11 GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 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_95 GBV_ILN_105 GBV_ILN_110 GBV_ILN_150 GBV_ILN_151 GBV_ILN_161 GBV_ILN_165 GBV_ILN_170 GBV_ILN_213 GBV_ILN_224 GBV_ILN_230 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_2001 GBV_ILN_2003 GBV_ILN_2004 GBV_ILN_2005 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_2038 GBV_ILN_2044 GBV_ILN_2048 GBV_ILN_2049 GBV_ILN_2050 GBV_ILN_2055 GBV_ILN_2056 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 GBV_ILN_2088 GBV_ILN_2106 GBV_ILN_2110 GBV_ILN_2111 GBV_ILN_2112 GBV_ILN_2118 GBV_ILN_2122 GBV_ILN_2129 GBV_ILN_2143 GBV_ILN_2147 GBV_ILN_2148 GBV_ILN_2152 GBV_ILN_2153 GBV_ILN_2190 GBV_ILN_2232 GBV_ILN_2336 GBV_ILN_2470 GBV_ILN_2472 GBV_ILN_2507 GBV_ILN_2548 GBV_ILN_4012 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4046 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4242 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_4338 GBV_ILN_4367 GBV_ILN_4393 GBV_ILN_4700 AR 196 2020 109190-
allfieldsSound	10.1016/j.matdes.2020.109190 doi (DE-627)DOAJ007037031 (DE-599)DOAJ5717b7e46e5e46a5b79cf74557409818 DE-627 ger DE-627 rakwb eng TA401-492 T.J. Bian verfasserin aut Through-thickness heterogeneity and in-plane anisotropy in creep aging of 7050 Al alloy 2020 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier During creep aging (CA), through-thickness heterogeneity and in-plane anisotropy in creep and mechanical properties affect the shape forming and performance tailoring. The specimens are first machined from the surface (t1), subsurface (t2) and center (t3) layers along the thickness direction of the 7050 Al alloy plate. Then in the rolling plane of each layer, the specimens are taken along the angles of 0° (L0), 45° (L45) and 90° (L90) to the rolling direction. After CA, the creep strain shows the trends of t1 < t2 < t3 along the thickness direction and L45 < L90 < L0 for in-plane directions, while the yield strength (YS) shows t1 < t3 < t2 and L90 < L0 < L45, respectively.Before CA, the low-angle grain boundaries (LAGBs) increase along the thickness direction, leading to a reduced creep strain. After CA, through-thickness heterogeneous LAGBs contributes to the above trend of YS. After L45 and L90 loading, S, Brass and Copper textures are obviously weaker than that under L0 loading, and show the largest equivalent Schmid factor (ESF) for L45 loading, and that for L0 and L90 conditions are approaching; while the equivalent slip system number (ESSN) shows L90 < L0 < L45. Both ESF and ESSN determine the in-plane anisotropy by affecting dislocation slip, but ESF plays a dominant role. Creep aging Through-thickness heterogeneity In-plane anisotropy Low angle grain boundary Texture 7050 Al alloy Materials of engineering and construction. Mechanics of materials H. Li verfasserin aut J.C. Yang verfasserin aut C. Lei verfasserin aut C.H. Wu verfasserin aut L.W. Zhang verfasserin aut G.Y. Chen verfasserin aut In Materials & Design Elsevier, 2019 196(2020), Seite 109190- (DE-627)32052857X (DE-600)2015480-X 18734197 nnns volume:196 year:2020 pages:109190- https://doi.org/10.1016/j.matdes.2020.109190 kostenfrei https://doaj.org/article/5717b7e46e5e46a5b79cf74557409818 kostenfrei http://www.sciencedirect.com/science/article/pii/S0264127520307255 kostenfrei https://doaj.org/toc/0264-1275 Journal toc kostenfrei GBV_USEFLAG_A SYSFLAG_A GBV_DOAJ SSG-OLC-PHA GBV_ILN_11 GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 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_95 GBV_ILN_105 GBV_ILN_110 GBV_ILN_150 GBV_ILN_151 GBV_ILN_161 GBV_ILN_165 GBV_ILN_170 GBV_ILN_213 GBV_ILN_224 GBV_ILN_230 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_2001 GBV_ILN_2003 GBV_ILN_2004 GBV_ILN_2005 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_2038 GBV_ILN_2044 GBV_ILN_2048 GBV_ILN_2049 GBV_ILN_2050 GBV_ILN_2055 GBV_ILN_2056 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 GBV_ILN_2088 GBV_ILN_2106 GBV_ILN_2110 GBV_ILN_2111 GBV_ILN_2112 GBV_ILN_2118 GBV_ILN_2122 GBV_ILN_2129 GBV_ILN_2143 GBV_ILN_2147 GBV_ILN_2148 GBV_ILN_2152 GBV_ILN_2153 GBV_ILN_2190 GBV_ILN_2232 GBV_ILN_2336 GBV_ILN_2470 GBV_ILN_2472 GBV_ILN_2507 GBV_ILN_2548 GBV_ILN_4012 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4046 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4242 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_4338 GBV_ILN_4367 GBV_ILN_4393 GBV_ILN_4700 AR 196 2020 109190-
language	English
source	In Materials & Design 196(2020), Seite 109190- volume:196 year:2020 pages:109190-
sourceStr	In Materials & Design 196(2020), Seite 109190- volume:196 year:2020 pages:109190-
format_phy_str_mv	Article
institution	findex.gbv.de
topic_facet	Creep aging Through-thickness heterogeneity In-plane anisotropy Low angle grain boundary Texture 7050 Al alloy Materials of engineering and construction. Mechanics of materials
isfreeaccess_bool	true
container_title	Materials & Design
authorswithroles_txt_mv	T.J. Bian @@aut@@ H. Li @@aut@@ J.C. Yang @@aut@@ C. Lei @@aut@@ C.H. Wu @@aut@@ L.W. Zhang @@aut@@ G.Y. Chen @@aut@@
publishDateDaySort_date	2020-01-01T00:00:00Z
hierarchy_top_id	32052857X
id	DOAJ007037031
language_de	englisch
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Bian</subfield><subfield code="e">verfasserin</subfield><subfield code="4">aut</subfield></datafield><datafield tag="245" ind1="1" ind2="0"><subfield code="a">Through-thickness heterogeneity and in-plane anisotropy in creep aging of 7050 Al alloy</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">During creep aging (CA), through-thickness heterogeneity and in-plane anisotropy in creep and mechanical properties affect the shape forming and performance tailoring. The specimens are first machined from the surface (t1), subsurface (t2) and center (t3) layers along the thickness direction of the 7050 Al alloy plate. Then in the rolling plane of each layer, the specimens are taken along the angles of 0° (L0), 45° (L45) and 90° (L90) to the rolling direction. After CA, the creep strain shows the trends of t1 < t2 < t3 along the thickness direction and L45 < L90 < L0 for in-plane directions, while the yield strength (YS) shows t1 < t3 < t2 and L90 < L0 < L45, respectively.Before CA, the low-angle grain boundaries (LAGBs) increase along the thickness direction, leading to a reduced creep strain. After CA, through-thickness heterogeneous LAGBs contributes to the above trend of YS. After L45 and L90 loading, S, Brass and Copper textures are obviously weaker than that under L0 loading, and show the largest equivalent Schmid factor (ESF) for L45 loading, and that for L0 and L90 conditions are approaching; while the equivalent slip system number (ESSN) shows L90 < L0 < L45. 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callnumber-first	T - Technology
author	T.J. Bian
spellingShingle	T.J. Bian misc TA401-492 misc Creep aging misc Through-thickness heterogeneity misc In-plane anisotropy misc Low angle grain boundary misc Texture misc 7050 Al alloy misc Materials of engineering and construction. Mechanics of materials Through-thickness heterogeneity and in-plane anisotropy in creep aging of 7050 Al alloy
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topic_title	TA401-492 Through-thickness heterogeneity and in-plane anisotropy in creep aging of 7050 Al alloy Creep aging Through-thickness heterogeneity In-plane anisotropy Low angle grain boundary Texture 7050 Al alloy
topic	misc TA401-492 misc Creep aging misc Through-thickness heterogeneity misc In-plane anisotropy misc Low angle grain boundary misc Texture misc 7050 Al alloy misc Materials of engineering and construction. Mechanics of materials
topic_unstemmed	misc TA401-492 misc Creep aging misc Through-thickness heterogeneity misc In-plane anisotropy misc Low angle grain boundary misc Texture misc 7050 Al alloy misc Materials of engineering and construction. Mechanics of materials
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title	Through-thickness heterogeneity and in-plane anisotropy in creep aging of 7050 Al alloy
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title_full	Through-thickness heterogeneity and in-plane anisotropy in creep aging of 7050 Al alloy
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author_browse	T.J. Bian H. Li J.C. Yang C. Lei C.H. Wu L.W. Zhang G.Y. Chen
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title_sort	through-thickness heterogeneity and in-plane anisotropy in creep aging of 7050 al alloy
callnumber	TA401-492
title_auth	Through-thickness heterogeneity and in-plane anisotropy in creep aging of 7050 Al alloy
abstract	During creep aging (CA), through-thickness heterogeneity and in-plane anisotropy in creep and mechanical properties affect the shape forming and performance tailoring. The specimens are first machined from the surface (t1), subsurface (t2) and center (t3) layers along the thickness direction of the 7050 Al alloy plate. Then in the rolling plane of each layer, the specimens are taken along the angles of 0° (L0), 45° (L45) and 90° (L90) to the rolling direction. After CA, the creep strain shows the trends of t1 < t2 < t3 along the thickness direction and L45 < L90 < L0 for in-plane directions, while the yield strength (YS) shows t1 < t3 < t2 and L90 < L0 < L45, respectively.Before CA, the low-angle grain boundaries (LAGBs) increase along the thickness direction, leading to a reduced creep strain. After CA, through-thickness heterogeneous LAGBs contributes to the above trend of YS. After L45 and L90 loading, S, Brass and Copper textures are obviously weaker than that under L0 loading, and show the largest equivalent Schmid factor (ESF) for L45 loading, and that for L0 and L90 conditions are approaching; while the equivalent slip system number (ESSN) shows L90 < L0 < L45. Both ESF and ESSN determine the in-plane anisotropy by affecting dislocation slip, but ESF plays a dominant role.
abstractGer	During creep aging (CA), through-thickness heterogeneity and in-plane anisotropy in creep and mechanical properties affect the shape forming and performance tailoring. The specimens are first machined from the surface (t1), subsurface (t2) and center (t3) layers along the thickness direction of the 7050 Al alloy plate. Then in the rolling plane of each layer, the specimens are taken along the angles of 0° (L0), 45° (L45) and 90° (L90) to the rolling direction. After CA, the creep strain shows the trends of t1 < t2 < t3 along the thickness direction and L45 < L90 < L0 for in-plane directions, while the yield strength (YS) shows t1 < t3 < t2 and L90 < L0 < L45, respectively.Before CA, the low-angle grain boundaries (LAGBs) increase along the thickness direction, leading to a reduced creep strain. After CA, through-thickness heterogeneous LAGBs contributes to the above trend of YS. After L45 and L90 loading, S, Brass and Copper textures are obviously weaker than that under L0 loading, and show the largest equivalent Schmid factor (ESF) for L45 loading, and that for L0 and L90 conditions are approaching; while the equivalent slip system number (ESSN) shows L90 < L0 < L45. Both ESF and ESSN determine the in-plane anisotropy by affecting dislocation slip, but ESF plays a dominant role.
abstract_unstemmed	During creep aging (CA), through-thickness heterogeneity and in-plane anisotropy in creep and mechanical properties affect the shape forming and performance tailoring. The specimens are first machined from the surface (t1), subsurface (t2) and center (t3) layers along the thickness direction of the 7050 Al alloy plate. Then in the rolling plane of each layer, the specimens are taken along the angles of 0° (L0), 45° (L45) and 90° (L90) to the rolling direction. After CA, the creep strain shows the trends of t1 < t2 < t3 along the thickness direction and L45 < L90 < L0 for in-plane directions, while the yield strength (YS) shows t1 < t3 < t2 and L90 < L0 < L45, respectively.Before CA, the low-angle grain boundaries (LAGBs) increase along the thickness direction, leading to a reduced creep strain. After CA, through-thickness heterogeneous LAGBs contributes to the above trend of YS. After L45 and L90 loading, S, Brass and Copper textures are obviously weaker than that under L0 loading, and show the largest equivalent Schmid factor (ESF) for L45 loading, and that for L0 and L90 conditions are approaching; while the equivalent slip system number (ESSN) shows L90 < L0 < L45. Both ESF and ESSN determine the in-plane anisotropy by affecting dislocation slip, but ESF plays a dominant role.
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title_short	Through-thickness heterogeneity and in-plane anisotropy in creep aging of 7050 Al alloy
url	https://doi.org/10.1016/j.matdes.2020.109190 https://doaj.org/article/5717b7e46e5e46a5b79cf74557409818 http://www.sciencedirect.com/science/article/pii/S0264127520307255 https://doaj.org/toc/0264-1275
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Bian</subfield><subfield code="e">verfasserin</subfield><subfield code="4">aut</subfield></datafield><datafield tag="245" ind1="1" ind2="0"><subfield code="a">Through-thickness heterogeneity and in-plane anisotropy in creep aging of 7050 Al alloy</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">During creep aging (CA), through-thickness heterogeneity and in-plane anisotropy in creep and mechanical properties affect the shape forming and performance tailoring. The specimens are first machined from the surface (t1), subsurface (t2) and center (t3) layers along the thickness direction of the 7050 Al alloy plate. Then in the rolling plane of each layer, the specimens are taken along the angles of 0° (L0), 45° (L45) and 90° (L90) to the rolling direction. After CA, the creep strain shows the trends of t1 < t2 < t3 along the thickness direction and L45 < L90 < L0 for in-plane directions, while the yield strength (YS) shows t1 < t3 < t2 and L90 < L0 < L45, respectively.Before CA, the low-angle grain boundaries (LAGBs) increase along the thickness direction, leading to a reduced creep strain. After CA, through-thickness heterogeneous LAGBs contributes to the above trend of YS. After L45 and L90 loading, S, Brass and Copper textures are obviously weaker than that under L0 loading, and show the largest equivalent Schmid factor (ESF) for L45 loading, and that for L0 and L90 conditions are approaching; while the equivalent slip system number (ESSN) shows L90 < L0 < L45. 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Through-thickness heterogeneity and in-plane anisotropy in creep aging of 7050 Al alloy

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