Evolution of microstructure and mechanical properties of C

The evolution of micro-morphology and physical properties of Cf/SiC-Al composites prepared by precursor impregnation and pyrolysis (PIP) and high-temperature pressure infiltration processes after high-temperature oxidation (300–700 °C) was investigated. Nanoindentation method was used to characteriz...
Ausführliche Beschreibung

Gespeichert in:

Autor*in:	Liao, Jiahao [verfasserIn] Yang, Lixia [verfasserIn] Chen, Zhaofeng [verfasserIn] Guan, Tianru [verfasserIn] Liu, Tianlong [verfasserIn]

Format:	E-Artikel
Sprache:	Englisch

Erschienen:	2022

Schlagwörter:	C High-temperature oxidation Nanoindentation Compressive strength Oxidative damage

Übergeordnetes Werk:	Enthalten in: Materials characterization - New York, NY : Science Direct, 1990, 194
Übergeordnetes Werk:	volume:194

DOI / URN:	10.1016/j.matchar.2022.112487

Katalog-ID:	ELV008868115

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520			\|a The evolution of micro-morphology and physical properties of Cf/SiC-Al composites prepared by precursor impregnation and pyrolysis (PIP) and high-temperature pressure infiltration processes after high-temperature oxidation (300–700 °C) was investigated. Nanoindentation method was used to characterize the hardness and elastic modulus of each component of the composites. The results demonstrated that with the increased of the oxidation temperature, the weight loss rate of the composites gradually increased, and in-plane compressive strength decreases gradually. The composites showed significant oxidation damage after the oxidation temperature exceeded 500 °C, and the nanoindentation hardness and elastic modulus of the Al alloy matrix were significantly reduced. After the oxidation treatment at 700 °C, the Al alloy matrix in the composites even melted and flowed out. The oxidative damage and compression fracture failure mechanisms of the composites after oxidation were also further discussed and analyzed.
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matchkey_str	liaojiahaoyanglixiachenzhaofengguantianr:2022----:vltoomcotutradehnc
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allfields	10.1016/j.matchar.2022.112487 doi (DE-627)ELV008868115 (ELSEVIER)S1044-5803(22)00769-0 DE-627 ger DE-627 rda eng 670 DE-600 51.30 bkl Liao, Jiahao verfasserin aut Evolution of microstructure and mechanical properties of C 2022 nicht spezifiziert zzz rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier The evolution of micro-morphology and physical properties of Cf/SiC-Al composites prepared by precursor impregnation and pyrolysis (PIP) and high-temperature pressure infiltration processes after high-temperature oxidation (300–700 °C) was investigated. Nanoindentation method was used to characterize the hardness and elastic modulus of each component of the composites. The results demonstrated that with the increased of the oxidation temperature, the weight loss rate of the composites gradually increased, and in-plane compressive strength decreases gradually. The composites showed significant oxidation damage after the oxidation temperature exceeded 500 °C, and the nanoindentation hardness and elastic modulus of the Al alloy matrix were significantly reduced. After the oxidation treatment at 700 °C, the Al alloy matrix in the composites even melted and flowed out. The oxidative damage and compression fracture failure mechanisms of the composites after oxidation were also further discussed and analyzed. C High-temperature oxidation Nanoindentation Compressive strength Oxidative damage Yang, Lixia verfasserin aut Chen, Zhaofeng verfasserin aut Guan, Tianru verfasserin aut Liu, Tianlong verfasserin aut Enthalten in Materials characterization New York, NY : Science Direct, 1990 194 Online-Ressource (DE-627)302719288 (DE-600)1491951-5 (DE-576)259483966 nnns volume:194 GBV_USEFLAG_U SYSFLAG_U GBV_ELV 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_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_150 GBV_ILN_151 GBV_ILN_224 GBV_ILN_370 GBV_ILN_602 GBV_ILN_702 GBV_ILN_2003 GBV_ILN_2004 GBV_ILN_2005 GBV_ILN_2008 GBV_ILN_2010 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_2025 GBV_ILN_2027 GBV_ILN_2034 GBV_ILN_2038 GBV_ILN_2044 GBV_ILN_2048 GBV_ILN_2049 GBV_ILN_2050 GBV_ILN_2056 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 GBV_ILN_2088 GBV_ILN_2111 GBV_ILN_2112 GBV_ILN_2113 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_2336 GBV_ILN_2470 GBV_ILN_2507 GBV_ILN_2522 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4046 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4242 GBV_ILN_4251 GBV_ILN_4305 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_4393 51.30 Werkstoffprüfung Werkstoffuntersuchung AR 194
spelling	10.1016/j.matchar.2022.112487 doi (DE-627)ELV008868115 (ELSEVIER)S1044-5803(22)00769-0 DE-627 ger DE-627 rda eng 670 DE-600 51.30 bkl Liao, Jiahao verfasserin aut Evolution of microstructure and mechanical properties of C 2022 nicht spezifiziert zzz rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier The evolution of micro-morphology and physical properties of Cf/SiC-Al composites prepared by precursor impregnation and pyrolysis (PIP) and high-temperature pressure infiltration processes after high-temperature oxidation (300–700 °C) was investigated. Nanoindentation method was used to characterize the hardness and elastic modulus of each component of the composites. The results demonstrated that with the increased of the oxidation temperature, the weight loss rate of the composites gradually increased, and in-plane compressive strength decreases gradually. The composites showed significant oxidation damage after the oxidation temperature exceeded 500 °C, and the nanoindentation hardness and elastic modulus of the Al alloy matrix were significantly reduced. After the oxidation treatment at 700 °C, the Al alloy matrix in the composites even melted and flowed out. The oxidative damage and compression fracture failure mechanisms of the composites after oxidation were also further discussed and analyzed. C High-temperature oxidation Nanoindentation Compressive strength Oxidative damage Yang, Lixia verfasserin aut Chen, Zhaofeng verfasserin aut Guan, Tianru verfasserin aut Liu, Tianlong verfasserin aut Enthalten in Materials characterization New York, NY : Science Direct, 1990 194 Online-Ressource (DE-627)302719288 (DE-600)1491951-5 (DE-576)259483966 nnns volume:194 GBV_USEFLAG_U SYSFLAG_U GBV_ELV 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_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_150 GBV_ILN_151 GBV_ILN_224 GBV_ILN_370 GBV_ILN_602 GBV_ILN_702 GBV_ILN_2003 GBV_ILN_2004 GBV_ILN_2005 GBV_ILN_2008 GBV_ILN_2010 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_2025 GBV_ILN_2027 GBV_ILN_2034 GBV_ILN_2038 GBV_ILN_2044 GBV_ILN_2048 GBV_ILN_2049 GBV_ILN_2050 GBV_ILN_2056 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 GBV_ILN_2088 GBV_ILN_2111 GBV_ILN_2112 GBV_ILN_2113 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_2336 GBV_ILN_2470 GBV_ILN_2507 GBV_ILN_2522 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4046 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4242 GBV_ILN_4251 GBV_ILN_4305 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_4393 51.30 Werkstoffprüfung Werkstoffuntersuchung AR 194
allfields_unstemmed	10.1016/j.matchar.2022.112487 doi (DE-627)ELV008868115 (ELSEVIER)S1044-5803(22)00769-0 DE-627 ger DE-627 rda eng 670 DE-600 51.30 bkl Liao, Jiahao verfasserin aut Evolution of microstructure and mechanical properties of C 2022 nicht spezifiziert zzz rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier The evolution of micro-morphology and physical properties of Cf/SiC-Al composites prepared by precursor impregnation and pyrolysis (PIP) and high-temperature pressure infiltration processes after high-temperature oxidation (300–700 °C) was investigated. Nanoindentation method was used to characterize the hardness and elastic modulus of each component of the composites. The results demonstrated that with the increased of the oxidation temperature, the weight loss rate of the composites gradually increased, and in-plane compressive strength decreases gradually. The composites showed significant oxidation damage after the oxidation temperature exceeded 500 °C, and the nanoindentation hardness and elastic modulus of the Al alloy matrix were significantly reduced. After the oxidation treatment at 700 °C, the Al alloy matrix in the composites even melted and flowed out. The oxidative damage and compression fracture failure mechanisms of the composites after oxidation were also further discussed and analyzed. C High-temperature oxidation Nanoindentation Compressive strength Oxidative damage Yang, Lixia verfasserin aut Chen, Zhaofeng verfasserin aut Guan, Tianru verfasserin aut Liu, Tianlong verfasserin aut Enthalten in Materials characterization New York, NY : Science Direct, 1990 194 Online-Ressource (DE-627)302719288 (DE-600)1491951-5 (DE-576)259483966 nnns volume:194 GBV_USEFLAG_U SYSFLAG_U GBV_ELV 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_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_150 GBV_ILN_151 GBV_ILN_224 GBV_ILN_370 GBV_ILN_602 GBV_ILN_702 GBV_ILN_2003 GBV_ILN_2004 GBV_ILN_2005 GBV_ILN_2008 GBV_ILN_2010 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_2025 GBV_ILN_2027 GBV_ILN_2034 GBV_ILN_2038 GBV_ILN_2044 GBV_ILN_2048 GBV_ILN_2049 GBV_ILN_2050 GBV_ILN_2056 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 GBV_ILN_2088 GBV_ILN_2111 GBV_ILN_2112 GBV_ILN_2113 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_2336 GBV_ILN_2470 GBV_ILN_2507 GBV_ILN_2522 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4046 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4242 GBV_ILN_4251 GBV_ILN_4305 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_4393 51.30 Werkstoffprüfung Werkstoffuntersuchung AR 194
allfieldsGer	10.1016/j.matchar.2022.112487 doi (DE-627)ELV008868115 (ELSEVIER)S1044-5803(22)00769-0 DE-627 ger DE-627 rda eng 670 DE-600 51.30 bkl Liao, Jiahao verfasserin aut Evolution of microstructure and mechanical properties of C 2022 nicht spezifiziert zzz rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier The evolution of micro-morphology and physical properties of Cf/SiC-Al composites prepared by precursor impregnation and pyrolysis (PIP) and high-temperature pressure infiltration processes after high-temperature oxidation (300–700 °C) was investigated. Nanoindentation method was used to characterize the hardness and elastic modulus of each component of the composites. The results demonstrated that with the increased of the oxidation temperature, the weight loss rate of the composites gradually increased, and in-plane compressive strength decreases gradually. The composites showed significant oxidation damage after the oxidation temperature exceeded 500 °C, and the nanoindentation hardness and elastic modulus of the Al alloy matrix were significantly reduced. After the oxidation treatment at 700 °C, the Al alloy matrix in the composites even melted and flowed out. The oxidative damage and compression fracture failure mechanisms of the composites after oxidation were also further discussed and analyzed. C High-temperature oxidation Nanoindentation Compressive strength Oxidative damage Yang, Lixia verfasserin aut Chen, Zhaofeng verfasserin aut Guan, Tianru verfasserin aut Liu, Tianlong verfasserin aut Enthalten in Materials characterization New York, NY : Science Direct, 1990 194 Online-Ressource (DE-627)302719288 (DE-600)1491951-5 (DE-576)259483966 nnns volume:194 GBV_USEFLAG_U SYSFLAG_U GBV_ELV 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_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_150 GBV_ILN_151 GBV_ILN_224 GBV_ILN_370 GBV_ILN_602 GBV_ILN_702 GBV_ILN_2003 GBV_ILN_2004 GBV_ILN_2005 GBV_ILN_2008 GBV_ILN_2010 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_2025 GBV_ILN_2027 GBV_ILN_2034 GBV_ILN_2038 GBV_ILN_2044 GBV_ILN_2048 GBV_ILN_2049 GBV_ILN_2050 GBV_ILN_2056 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 GBV_ILN_2088 GBV_ILN_2111 GBV_ILN_2112 GBV_ILN_2113 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_2336 GBV_ILN_2470 GBV_ILN_2507 GBV_ILN_2522 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4046 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4242 GBV_ILN_4251 GBV_ILN_4305 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_4393 51.30 Werkstoffprüfung Werkstoffuntersuchung AR 194
allfieldsSound	10.1016/j.matchar.2022.112487 doi (DE-627)ELV008868115 (ELSEVIER)S1044-5803(22)00769-0 DE-627 ger DE-627 rda eng 670 DE-600 51.30 bkl Liao, Jiahao verfasserin aut Evolution of microstructure and mechanical properties of C 2022 nicht spezifiziert zzz rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier The evolution of micro-morphology and physical properties of Cf/SiC-Al composites prepared by precursor impregnation and pyrolysis (PIP) and high-temperature pressure infiltration processes after high-temperature oxidation (300–700 °C) was investigated. Nanoindentation method was used to characterize the hardness and elastic modulus of each component of the composites. The results demonstrated that with the increased of the oxidation temperature, the weight loss rate of the composites gradually increased, and in-plane compressive strength decreases gradually. The composites showed significant oxidation damage after the oxidation temperature exceeded 500 °C, and the nanoindentation hardness and elastic modulus of the Al alloy matrix were significantly reduced. After the oxidation treatment at 700 °C, the Al alloy matrix in the composites even melted and flowed out. The oxidative damage and compression fracture failure mechanisms of the composites after oxidation were also further discussed and analyzed. C High-temperature oxidation Nanoindentation Compressive strength Oxidative damage Yang, Lixia verfasserin aut Chen, Zhaofeng verfasserin aut Guan, Tianru verfasserin aut Liu, Tianlong verfasserin aut Enthalten in Materials characterization New York, NY : Science Direct, 1990 194 Online-Ressource (DE-627)302719288 (DE-600)1491951-5 (DE-576)259483966 nnns volume:194 GBV_USEFLAG_U SYSFLAG_U GBV_ELV 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_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_150 GBV_ILN_151 GBV_ILN_224 GBV_ILN_370 GBV_ILN_602 GBV_ILN_702 GBV_ILN_2003 GBV_ILN_2004 GBV_ILN_2005 GBV_ILN_2008 GBV_ILN_2010 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_2025 GBV_ILN_2027 GBV_ILN_2034 GBV_ILN_2038 GBV_ILN_2044 GBV_ILN_2048 GBV_ILN_2049 GBV_ILN_2050 GBV_ILN_2056 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 GBV_ILN_2088 GBV_ILN_2111 GBV_ILN_2112 GBV_ILN_2113 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_2336 GBV_ILN_2470 GBV_ILN_2507 GBV_ILN_2522 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4046 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4242 GBV_ILN_4251 GBV_ILN_4305 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_4393 51.30 Werkstoffprüfung Werkstoffuntersuchung AR 194
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topic_facet	C High-temperature oxidation Nanoindentation Compressive strength Oxidative damage
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author	Liao, Jiahao
spellingShingle	Liao, Jiahao ddc 670 bkl 51.30 misc C misc High-temperature oxidation misc Nanoindentation misc Compressive strength misc Oxidative damage Evolution of microstructure and mechanical properties of C
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topic_title	670 DE-600 51.30 bkl Evolution of microstructure and mechanical properties of C C High-temperature oxidation Nanoindentation Compressive strength Oxidative damage
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title	Evolution of microstructure and mechanical properties of C
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title_full	Evolution of microstructure and mechanical properties of C
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title_sort	evolution of microstructure and mechanical properties of c
title_auth	Evolution of microstructure and mechanical properties of C
abstract	The evolution of micro-morphology and physical properties of Cf/SiC-Al composites prepared by precursor impregnation and pyrolysis (PIP) and high-temperature pressure infiltration processes after high-temperature oxidation (300–700 °C) was investigated. Nanoindentation method was used to characterize the hardness and elastic modulus of each component of the composites. The results demonstrated that with the increased of the oxidation temperature, the weight loss rate of the composites gradually increased, and in-plane compressive strength decreases gradually. The composites showed significant oxidation damage after the oxidation temperature exceeded 500 °C, and the nanoindentation hardness and elastic modulus of the Al alloy matrix were significantly reduced. After the oxidation treatment at 700 °C, the Al alloy matrix in the composites even melted and flowed out. The oxidative damage and compression fracture failure mechanisms of the composites after oxidation were also further discussed and analyzed.
abstractGer	The evolution of micro-morphology and physical properties of Cf/SiC-Al composites prepared by precursor impregnation and pyrolysis (PIP) and high-temperature pressure infiltration processes after high-temperature oxidation (300–700 °C) was investigated. Nanoindentation method was used to characterize the hardness and elastic modulus of each component of the composites. The results demonstrated that with the increased of the oxidation temperature, the weight loss rate of the composites gradually increased, and in-plane compressive strength decreases gradually. The composites showed significant oxidation damage after the oxidation temperature exceeded 500 °C, and the nanoindentation hardness and elastic modulus of the Al alloy matrix were significantly reduced. After the oxidation treatment at 700 °C, the Al alloy matrix in the composites even melted and flowed out. The oxidative damage and compression fracture failure mechanisms of the composites after oxidation were also further discussed and analyzed.
abstract_unstemmed	The evolution of micro-morphology and physical properties of Cf/SiC-Al composites prepared by precursor impregnation and pyrolysis (PIP) and high-temperature pressure infiltration processes after high-temperature oxidation (300–700 °C) was investigated. Nanoindentation method was used to characterize the hardness and elastic modulus of each component of the composites. The results demonstrated that with the increased of the oxidation temperature, the weight loss rate of the composites gradually increased, and in-plane compressive strength decreases gradually. The composites showed significant oxidation damage after the oxidation temperature exceeded 500 °C, and the nanoindentation hardness and elastic modulus of the Al alloy matrix were significantly reduced. After the oxidation treatment at 700 °C, the Al alloy matrix in the composites even melted and flowed out. The oxidative damage and compression fracture failure mechanisms of the composites after oxidation were also further discussed and analyzed.
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title_short	Evolution of microstructure and mechanical properties of C
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author2	Yang, Lixia Chen, Zhaofeng Guan, Tianru Liu, Tianlong
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doi_str	10.1016/j.matchar.2022.112487
up_date	2024-07-06T21:10:53.665Z
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