Micro-CT based parametric modeling and damage analysis of three-dimensional rotary-five-directional braided composites under tensile load

Three-dimensional (3D) braided composites have broad applications in aviation and aerospace fields due to their outstanding mechanical properties. However, the damage mechanism of 3D braided composites fabricated by rotary braided composites is still unclear. In this paper, a parametric finite eleme...
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Gespeichert in:

Autor*in:	Li, Zhi-Jian [verfasserIn] Dai, Hong-Liang [verfasserIn] Liu, Zheng-Guo [verfasserIn] Wang, Ya [verfasserIn]

Format:	E-Artikel
Sprache:	Englisch

Erschienen:	2023

Schlagwörter:	3D braided composites Rotary braiding Parametric finite element modeling Micro-CT Damage mechanism

Übergeordnetes Werk:	Enthalten in: Composite structures - Amsterdam : Elsevier, 1983, 309
Übergeordnetes Werk:	volume:309

DOI / URN:	10.1016/j.compstruct.2023.116734

Katalog-ID:	ELV009251391

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520			\|a Three-dimensional (3D) braided composites have broad applications in aviation and aerospace fields due to their outstanding mechanical properties. However, the damage mechanism of 3D braided composites fabricated by rotary braided composites is still unclear. In this paper, a parametric finite element modeling of 3D rotary-five-directional (3DR5d) braided composites is established, considering the realistic yarn cross-section based on a Micro-CT scan. A systematical approach for damage prediction is developed to analyze the damage behaviors of 3DR5d braided composites. The tensile mechanical properties and damage evolution of 3DR5d braided composites are predicted based on the proposed method. The accuracy of the proposed model is verified by the comparison with the data in the literature. The effect of braiding angles and fiber volume fractions on the mechanical properties and damage mechanisms of 3DR5d braided composites is investigated based on parametric analysis. The results show that the strength and modulus of 3DR5d braided composites increase with the decreasing braiding angle and the increasing fiber volume fractions. Moreover, transverse shear gradually dominates in the failure of 3DR5d braided composites in the tension process. The results could be beneficial to guide the design and fabrication of 3DR5d braided composites.
650		4	\|a 3D braided composites
650		4	\|a Rotary braiding
650		4	\|a Parametric finite element modeling
650		4	\|a Micro-CT
650		4	\|a Damage mechanism
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700	1		\|a Liu, Zheng-Guo \|e verfasserin \|4 aut
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allfields	10.1016/j.compstruct.2023.116734 doi (DE-627)ELV009251391 (ELSEVIER)S0263-8223(23)00078-8 DE-627 ger DE-627 rda eng 670 VZ 51.75 bkl Li, Zhi-Jian verfasserin aut Micro-CT based parametric modeling and damage analysis of three-dimensional rotary-five-directional braided composites under tensile load 2023 nicht spezifiziert zzz rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier Three-dimensional (3D) braided composites have broad applications in aviation and aerospace fields due to their outstanding mechanical properties. However, the damage mechanism of 3D braided composites fabricated by rotary braided composites is still unclear. In this paper, a parametric finite element modeling of 3D rotary-five-directional (3DR5d) braided composites is established, considering the realistic yarn cross-section based on a Micro-CT scan. A systematical approach for damage prediction is developed to analyze the damage behaviors of 3DR5d braided composites. The tensile mechanical properties and damage evolution of 3DR5d braided composites are predicted based on the proposed method. The accuracy of the proposed model is verified by the comparison with the data in the literature. The effect of braiding angles and fiber volume fractions on the mechanical properties and damage mechanisms of 3DR5d braided composites is investigated based on parametric analysis. The results show that the strength and modulus of 3DR5d braided composites increase with the decreasing braiding angle and the increasing fiber volume fractions. Moreover, transverse shear gradually dominates in the failure of 3DR5d braided composites in the tension process. The results could be beneficial to guide the design and fabrication of 3DR5d braided composites. 3D braided composites Rotary braiding Parametric finite element modeling Micro-CT Damage mechanism Dai, Hong-Liang verfasserin aut Liu, Zheng-Guo verfasserin aut Wang, Ya verfasserin aut Enthalten in Composite structures Amsterdam : Elsevier, 1983 309 (DE-627)320509044 (DE-600)2013177-X (DE-576)094531447 0263-8223 nnns volume:309 GBV_USEFLAG_U GBV_ELV SYSFLAG_U GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_32 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 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_150 GBV_ILN_151 GBV_ILN_187 GBV_ILN_213 GBV_ILN_224 GBV_ILN_230 GBV_ILN_370 GBV_ILN_602 GBV_ILN_702 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_2034 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_2088 GBV_ILN_2106 GBV_ILN_2110 GBV_ILN_2111 GBV_ILN_2112 GBV_ILN_2122 GBV_ILN_2129 GBV_ILN_2143 GBV_ILN_2152 GBV_ILN_2153 GBV_ILN_2190 GBV_ILN_2232 GBV_ILN_2336 GBV_ILN_2470 GBV_ILN_2507 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4112 GBV_ILN_4125 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_4338 GBV_ILN_4393 GBV_ILN_4700 51.75 Verbundwerkstoffe Schichtstoffe VZ AR 309
spelling	10.1016/j.compstruct.2023.116734 doi (DE-627)ELV009251391 (ELSEVIER)S0263-8223(23)00078-8 DE-627 ger DE-627 rda eng 670 VZ 51.75 bkl Li, Zhi-Jian verfasserin aut Micro-CT based parametric modeling and damage analysis of three-dimensional rotary-five-directional braided composites under tensile load 2023 nicht spezifiziert zzz rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier Three-dimensional (3D) braided composites have broad applications in aviation and aerospace fields due to their outstanding mechanical properties. However, the damage mechanism of 3D braided composites fabricated by rotary braided composites is still unclear. In this paper, a parametric finite element modeling of 3D rotary-five-directional (3DR5d) braided composites is established, considering the realistic yarn cross-section based on a Micro-CT scan. A systematical approach for damage prediction is developed to analyze the damage behaviors of 3DR5d braided composites. The tensile mechanical properties and damage evolution of 3DR5d braided composites are predicted based on the proposed method. The accuracy of the proposed model is verified by the comparison with the data in the literature. The effect of braiding angles and fiber volume fractions on the mechanical properties and damage mechanisms of 3DR5d braided composites is investigated based on parametric analysis. The results show that the strength and modulus of 3DR5d braided composites increase with the decreasing braiding angle and the increasing fiber volume fractions. Moreover, transverse shear gradually dominates in the failure of 3DR5d braided composites in the tension process. The results could be beneficial to guide the design and fabrication of 3DR5d braided composites. 3D braided composites Rotary braiding Parametric finite element modeling Micro-CT Damage mechanism Dai, Hong-Liang verfasserin aut Liu, Zheng-Guo verfasserin aut Wang, Ya verfasserin aut Enthalten in Composite structures Amsterdam : Elsevier, 1983 309 (DE-627)320509044 (DE-600)2013177-X (DE-576)094531447 0263-8223 nnns volume:309 GBV_USEFLAG_U GBV_ELV SYSFLAG_U GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_32 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 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_150 GBV_ILN_151 GBV_ILN_187 GBV_ILN_213 GBV_ILN_224 GBV_ILN_230 GBV_ILN_370 GBV_ILN_602 GBV_ILN_702 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_2034 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_2088 GBV_ILN_2106 GBV_ILN_2110 GBV_ILN_2111 GBV_ILN_2112 GBV_ILN_2122 GBV_ILN_2129 GBV_ILN_2143 GBV_ILN_2152 GBV_ILN_2153 GBV_ILN_2190 GBV_ILN_2232 GBV_ILN_2336 GBV_ILN_2470 GBV_ILN_2507 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4112 GBV_ILN_4125 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_4338 GBV_ILN_4393 GBV_ILN_4700 51.75 Verbundwerkstoffe Schichtstoffe VZ AR 309
allfields_unstemmed	10.1016/j.compstruct.2023.116734 doi (DE-627)ELV009251391 (ELSEVIER)S0263-8223(23)00078-8 DE-627 ger DE-627 rda eng 670 VZ 51.75 bkl Li, Zhi-Jian verfasserin aut Micro-CT based parametric modeling and damage analysis of three-dimensional rotary-five-directional braided composites under tensile load 2023 nicht spezifiziert zzz rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier Three-dimensional (3D) braided composites have broad applications in aviation and aerospace fields due to their outstanding mechanical properties. However, the damage mechanism of 3D braided composites fabricated by rotary braided composites is still unclear. In this paper, a parametric finite element modeling of 3D rotary-five-directional (3DR5d) braided composites is established, considering the realistic yarn cross-section based on a Micro-CT scan. A systematical approach for damage prediction is developed to analyze the damage behaviors of 3DR5d braided composites. The tensile mechanical properties and damage evolution of 3DR5d braided composites are predicted based on the proposed method. The accuracy of the proposed model is verified by the comparison with the data in the literature. The effect of braiding angles and fiber volume fractions on the mechanical properties and damage mechanisms of 3DR5d braided composites is investigated based on parametric analysis. The results show that the strength and modulus of 3DR5d braided composites increase with the decreasing braiding angle and the increasing fiber volume fractions. Moreover, transverse shear gradually dominates in the failure of 3DR5d braided composites in the tension process. The results could be beneficial to guide the design and fabrication of 3DR5d braided composites. 3D braided composites Rotary braiding Parametric finite element modeling Micro-CT Damage mechanism Dai, Hong-Liang verfasserin aut Liu, Zheng-Guo verfasserin aut Wang, Ya verfasserin aut Enthalten in Composite structures Amsterdam : Elsevier, 1983 309 (DE-627)320509044 (DE-600)2013177-X (DE-576)094531447 0263-8223 nnns volume:309 GBV_USEFLAG_U GBV_ELV SYSFLAG_U GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_32 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 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_150 GBV_ILN_151 GBV_ILN_187 GBV_ILN_213 GBV_ILN_224 GBV_ILN_230 GBV_ILN_370 GBV_ILN_602 GBV_ILN_702 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_2034 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_2088 GBV_ILN_2106 GBV_ILN_2110 GBV_ILN_2111 GBV_ILN_2112 GBV_ILN_2122 GBV_ILN_2129 GBV_ILN_2143 GBV_ILN_2152 GBV_ILN_2153 GBV_ILN_2190 GBV_ILN_2232 GBV_ILN_2336 GBV_ILN_2470 GBV_ILN_2507 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4112 GBV_ILN_4125 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_4338 GBV_ILN_4393 GBV_ILN_4700 51.75 Verbundwerkstoffe Schichtstoffe VZ AR 309
allfieldsGer	10.1016/j.compstruct.2023.116734 doi (DE-627)ELV009251391 (ELSEVIER)S0263-8223(23)00078-8 DE-627 ger DE-627 rda eng 670 VZ 51.75 bkl Li, Zhi-Jian verfasserin aut Micro-CT based parametric modeling and damage analysis of three-dimensional rotary-five-directional braided composites under tensile load 2023 nicht spezifiziert zzz rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier Three-dimensional (3D) braided composites have broad applications in aviation and aerospace fields due to their outstanding mechanical properties. However, the damage mechanism of 3D braided composites fabricated by rotary braided composites is still unclear. In this paper, a parametric finite element modeling of 3D rotary-five-directional (3DR5d) braided composites is established, considering the realistic yarn cross-section based on a Micro-CT scan. A systematical approach for damage prediction is developed to analyze the damage behaviors of 3DR5d braided composites. The tensile mechanical properties and damage evolution of 3DR5d braided composites are predicted based on the proposed method. The accuracy of the proposed model is verified by the comparison with the data in the literature. The effect of braiding angles and fiber volume fractions on the mechanical properties and damage mechanisms of 3DR5d braided composites is investigated based on parametric analysis. The results show that the strength and modulus of 3DR5d braided composites increase with the decreasing braiding angle and the increasing fiber volume fractions. Moreover, transverse shear gradually dominates in the failure of 3DR5d braided composites in the tension process. The results could be beneficial to guide the design and fabrication of 3DR5d braided composites. 3D braided composites Rotary braiding Parametric finite element modeling Micro-CT Damage mechanism Dai, Hong-Liang verfasserin aut Liu, Zheng-Guo verfasserin aut Wang, Ya verfasserin aut Enthalten in Composite structures Amsterdam : Elsevier, 1983 309 (DE-627)320509044 (DE-600)2013177-X (DE-576)094531447 0263-8223 nnns volume:309 GBV_USEFLAG_U GBV_ELV SYSFLAG_U GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_32 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 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_150 GBV_ILN_151 GBV_ILN_187 GBV_ILN_213 GBV_ILN_224 GBV_ILN_230 GBV_ILN_370 GBV_ILN_602 GBV_ILN_702 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_2034 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_2088 GBV_ILN_2106 GBV_ILN_2110 GBV_ILN_2111 GBV_ILN_2112 GBV_ILN_2122 GBV_ILN_2129 GBV_ILN_2143 GBV_ILN_2152 GBV_ILN_2153 GBV_ILN_2190 GBV_ILN_2232 GBV_ILN_2336 GBV_ILN_2470 GBV_ILN_2507 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4112 GBV_ILN_4125 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_4338 GBV_ILN_4393 GBV_ILN_4700 51.75 Verbundwerkstoffe Schichtstoffe VZ AR 309
allfieldsSound	10.1016/j.compstruct.2023.116734 doi (DE-627)ELV009251391 (ELSEVIER)S0263-8223(23)00078-8 DE-627 ger DE-627 rda eng 670 VZ 51.75 bkl Li, Zhi-Jian verfasserin aut Micro-CT based parametric modeling and damage analysis of three-dimensional rotary-five-directional braided composites under tensile load 2023 nicht spezifiziert zzz rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier Three-dimensional (3D) braided composites have broad applications in aviation and aerospace fields due to their outstanding mechanical properties. However, the damage mechanism of 3D braided composites fabricated by rotary braided composites is still unclear. In this paper, a parametric finite element modeling of 3D rotary-five-directional (3DR5d) braided composites is established, considering the realistic yarn cross-section based on a Micro-CT scan. A systematical approach for damage prediction is developed to analyze the damage behaviors of 3DR5d braided composites. The tensile mechanical properties and damage evolution of 3DR5d braided composites are predicted based on the proposed method. The accuracy of the proposed model is verified by the comparison with the data in the literature. The effect of braiding angles and fiber volume fractions on the mechanical properties and damage mechanisms of 3DR5d braided composites is investigated based on parametric analysis. The results show that the strength and modulus of 3DR5d braided composites increase with the decreasing braiding angle and the increasing fiber volume fractions. Moreover, transverse shear gradually dominates in the failure of 3DR5d braided composites in the tension process. The results could be beneficial to guide the design and fabrication of 3DR5d braided composites. 3D braided composites Rotary braiding Parametric finite element modeling Micro-CT Damage mechanism Dai, Hong-Liang verfasserin aut Liu, Zheng-Guo verfasserin aut Wang, Ya verfasserin aut Enthalten in Composite structures Amsterdam : Elsevier, 1983 309 (DE-627)320509044 (DE-600)2013177-X (DE-576)094531447 0263-8223 nnns volume:309 GBV_USEFLAG_U GBV_ELV SYSFLAG_U GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_32 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 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_150 GBV_ILN_151 GBV_ILN_187 GBV_ILN_213 GBV_ILN_224 GBV_ILN_230 GBV_ILN_370 GBV_ILN_602 GBV_ILN_702 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_2034 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_2088 GBV_ILN_2106 GBV_ILN_2110 GBV_ILN_2111 GBV_ILN_2112 GBV_ILN_2122 GBV_ILN_2129 GBV_ILN_2143 GBV_ILN_2152 GBV_ILN_2153 GBV_ILN_2190 GBV_ILN_2232 GBV_ILN_2336 GBV_ILN_2470 GBV_ILN_2507 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4112 GBV_ILN_4125 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_4338 GBV_ILN_4393 GBV_ILN_4700 51.75 Verbundwerkstoffe Schichtstoffe VZ AR 309
language	English
source	Enthalten in Composite structures 309 volume:309
sourceStr	Enthalten in Composite structures 309 volume:309
format_phy_str_mv	Article
bklname	Verbundwerkstoffe Schichtstoffe
institution	findex.gbv.de
topic_facet	3D braided composites Rotary braiding Parametric finite element modeling Micro-CT Damage mechanism
dewey-raw	670
isfreeaccess_bool	false
container_title	Composite structures
authorswithroles_txt_mv	Li, Zhi-Jian @@aut@@ Dai, Hong-Liang @@aut@@ Liu, Zheng-Guo @@aut@@ Wang, Ya @@aut@@
publishDateDaySort_date	2023-01-01T00:00:00Z
hierarchy_top_id	320509044
dewey-sort	3670
id	ELV009251391
language_de	englisch
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author	Li, Zhi-Jian
spellingShingle	Li, Zhi-Jian ddc 670 bkl 51.75 misc 3D braided composites misc Rotary braiding misc Parametric finite element modeling misc Micro-CT misc Damage mechanism Micro-CT based parametric modeling and damage analysis of three-dimensional rotary-five-directional braided composites under tensile load
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topic_title	670 VZ 51.75 bkl Micro-CT based parametric modeling and damage analysis of three-dimensional rotary-five-directional braided composites under tensile load 3D braided composites Rotary braiding Parametric finite element modeling Micro-CT Damage mechanism
topic	ddc 670 bkl 51.75 misc 3D braided composites misc Rotary braiding misc Parametric finite element modeling misc Micro-CT misc Damage mechanism
topic_unstemmed	ddc 670 bkl 51.75 misc 3D braided composites misc Rotary braiding misc Parametric finite element modeling misc Micro-CT misc Damage mechanism
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title	Micro-CT based parametric modeling and damage analysis of three-dimensional rotary-five-directional braided composites under tensile load
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title_full	Micro-CT based parametric modeling and damage analysis of three-dimensional rotary-five-directional braided composites under tensile load
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title_sort	micro-ct based parametric modeling and damage analysis of three-dimensional rotary-five-directional braided composites under tensile load
title_auth	Micro-CT based parametric modeling and damage analysis of three-dimensional rotary-five-directional braided composites under tensile load
abstract	Three-dimensional (3D) braided composites have broad applications in aviation and aerospace fields due to their outstanding mechanical properties. However, the damage mechanism of 3D braided composites fabricated by rotary braided composites is still unclear. In this paper, a parametric finite element modeling of 3D rotary-five-directional (3DR5d) braided composites is established, considering the realistic yarn cross-section based on a Micro-CT scan. A systematical approach for damage prediction is developed to analyze the damage behaviors of 3DR5d braided composites. The tensile mechanical properties and damage evolution of 3DR5d braided composites are predicted based on the proposed method. The accuracy of the proposed model is verified by the comparison with the data in the literature. The effect of braiding angles and fiber volume fractions on the mechanical properties and damage mechanisms of 3DR5d braided composites is investigated based on parametric analysis. The results show that the strength and modulus of 3DR5d braided composites increase with the decreasing braiding angle and the increasing fiber volume fractions. Moreover, transverse shear gradually dominates in the failure of 3DR5d braided composites in the tension process. The results could be beneficial to guide the design and fabrication of 3DR5d braided composites.
abstractGer	Three-dimensional (3D) braided composites have broad applications in aviation and aerospace fields due to their outstanding mechanical properties. However, the damage mechanism of 3D braided composites fabricated by rotary braided composites is still unclear. In this paper, a parametric finite element modeling of 3D rotary-five-directional (3DR5d) braided composites is established, considering the realistic yarn cross-section based on a Micro-CT scan. A systematical approach for damage prediction is developed to analyze the damage behaviors of 3DR5d braided composites. The tensile mechanical properties and damage evolution of 3DR5d braided composites are predicted based on the proposed method. The accuracy of the proposed model is verified by the comparison with the data in the literature. The effect of braiding angles and fiber volume fractions on the mechanical properties and damage mechanisms of 3DR5d braided composites is investigated based on parametric analysis. The results show that the strength and modulus of 3DR5d braided composites increase with the decreasing braiding angle and the increasing fiber volume fractions. Moreover, transverse shear gradually dominates in the failure of 3DR5d braided composites in the tension process. The results could be beneficial to guide the design and fabrication of 3DR5d braided composites.
abstract_unstemmed	Three-dimensional (3D) braided composites have broad applications in aviation and aerospace fields due to their outstanding mechanical properties. However, the damage mechanism of 3D braided composites fabricated by rotary braided composites is still unclear. In this paper, a parametric finite element modeling of 3D rotary-five-directional (3DR5d) braided composites is established, considering the realistic yarn cross-section based on a Micro-CT scan. A systematical approach for damage prediction is developed to analyze the damage behaviors of 3DR5d braided composites. The tensile mechanical properties and damage evolution of 3DR5d braided composites are predicted based on the proposed method. The accuracy of the proposed model is verified by the comparison with the data in the literature. The effect of braiding angles and fiber volume fractions on the mechanical properties and damage mechanisms of 3DR5d braided composites is investigated based on parametric analysis. The results show that the strength and modulus of 3DR5d braided composites increase with the decreasing braiding angle and the increasing fiber volume fractions. Moreover, transverse shear gradually dominates in the failure of 3DR5d braided composites in the tension process. The results could be beneficial to guide the design and fabrication of 3DR5d braided composites.
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title_short	Micro-CT based parametric modeling and damage analysis of three-dimensional rotary-five-directional braided composites under tensile load
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up_date	2024-07-06T22:31:24.097Z
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Micro-CT based parametric modeling and damage analysis of three-dimensional rotary-five-directional braided composites under tensile load

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