Anisotropy of radiation-induced degradation in mechanical properties of fabric-reinforced polymer-matrix composites
Abstract Four kinds of fabric-reinforced polymer-matrix composites (filler: E-glass or carbon fabric; matrix: epoxy or polyimide resin) were irradiated $ with^{60} $Coγ-rays or 2 MeV electrons at room temperature. Three-point bend tests were then carried out at 77 K and at room temperature in a 45°...
Ausführliche Beschreibung
Gespeichert in:
| Autor*in: |
Egusa, S. [verfasserIn] |
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| Format: |
Artikel |
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| Sprache: |
Englisch |
| Erschienen: |
1990 |
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| Schlagwörter: |
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| Anmerkung: |
© Chapman and Hall Ltd 1990 |
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| Übergeordnetes Werk: |
Enthalten in: Journal of materials science - Kluwer Academic Publishers, 1966, 25(1990), 3 vom: März, Seite 1863-1871 |
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| Übergeordnetes Werk: |
volume:25 ; year:1990 ; number:3 ; month:03 ; pages:1863-1871 |
| Links: |
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| DOI / URN: |
10.1007/BF01045398 |
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| Katalog-ID: |
OLC2046167384 |
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| 520 | |a Abstract Four kinds of fabric-reinforced polymer-matrix composites (filler: E-glass or carbon fabric; matrix: epoxy or polyimide resin) were irradiated $ with^{60} $Coγ-rays or 2 MeV electrons at room temperature. Three-point bend tests were then carried out at 77 K and at room temperature in a 45° direction from warp to fill. Comparison of the degradation behaviour among these composites reveals that the glass-epoxy and glass-polyimide composites are quite similar to each other in the dose dependence of the ultimate interlaminar shear strength at each test temperature. This result suggests that the radiation damage at the fibre-matrix interface decreases the contribution of the chemical bond mode to the total bond strength at the interface, thus decreasing the composite shear strength with increasing dose. For the carbon-epoxy and carbon-polyimide composites, on the other hand, the shear strength at room temperature changes little even after irradiation up to 140 MGy, while the shear strength at 77 K decreases monotonically with increasing dose. These findings suggest that the fibre-matrix bond strength due to the friction force mode is quite insensitive to radiation, thus resulting in the dose-independent shear strength at room temperature. At 77 K, however, the friction force mode fails to function properly because of the brittleness of the matrix resin, and consequently the composite shear strength decreases with increasing dose owing to a resulting increase in the matrix brittleness. | ||
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| 650 | 4 | |a Bond Strength | |
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| 650 | 4 | |a Degradation Behaviour | |
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10.1007/BF01045398 doi (DE-627)OLC2046167384 (DE-He213)BF01045398-p DE-627 ger DE-627 rakwb eng 670 VZ Egusa, S. verfasserin aut Anisotropy of radiation-induced degradation in mechanical properties of fabric-reinforced polymer-matrix composites 1990 Text txt rdacontent ohne Hilfsmittel zu benutzen n rdamedia Band nc rdacarrier © Chapman and Hall Ltd 1990 Abstract Four kinds of fabric-reinforced polymer-matrix composites (filler: E-glass or carbon fabric; matrix: epoxy or polyimide resin) were irradiated $ with^{60} $Coγ-rays or 2 MeV electrons at room temperature. Three-point bend tests were then carried out at 77 K and at room temperature in a 45° direction from warp to fill. Comparison of the degradation behaviour among these composites reveals that the glass-epoxy and glass-polyimide composites are quite similar to each other in the dose dependence of the ultimate interlaminar shear strength at each test temperature. This result suggests that the radiation damage at the fibre-matrix interface decreases the contribution of the chemical bond mode to the total bond strength at the interface, thus decreasing the composite shear strength with increasing dose. For the carbon-epoxy and carbon-polyimide composites, on the other hand, the shear strength at room temperature changes little even after irradiation up to 140 MGy, while the shear strength at 77 K decreases monotonically with increasing dose. These findings suggest that the fibre-matrix bond strength due to the friction force mode is quite insensitive to radiation, thus resulting in the dose-independent shear strength at room temperature. At 77 K, however, the friction force mode fails to function properly because of the brittleness of the matrix resin, and consequently the composite shear strength decreases with increasing dose owing to a resulting increase in the matrix brittleness. Shear Strength Bond Strength Polyimide Degradation Behaviour Matrix Resin Enthalten in Journal of materials science Kluwer Academic Publishers, 1966 25(1990), 3 vom: März, Seite 1863-1871 (DE-627)129546372 (DE-600)218324-9 (DE-576)014996774 0022-2461 nnns volume:25 year:1990 number:3 month:03 pages:1863-1871 https://doi.org/10.1007/BF01045398 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_OLC SSG-OLC-TEC GBV_ILN_11 GBV_ILN_20 GBV_ILN_23 GBV_ILN_30 GBV_ILN_32 GBV_ILN_40 GBV_ILN_62 GBV_ILN_65 GBV_ILN_70 GBV_ILN_2004 GBV_ILN_2006 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_2057 GBV_ILN_4082 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4316 GBV_ILN_4319 GBV_ILN_4323 GBV_ILN_4700 AR 25 1990 3 03 1863-1871 |
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10.1007/BF01045398 doi (DE-627)OLC2046167384 (DE-He213)BF01045398-p DE-627 ger DE-627 rakwb eng 670 VZ Egusa, S. verfasserin aut Anisotropy of radiation-induced degradation in mechanical properties of fabric-reinforced polymer-matrix composites 1990 Text txt rdacontent ohne Hilfsmittel zu benutzen n rdamedia Band nc rdacarrier © Chapman and Hall Ltd 1990 Abstract Four kinds of fabric-reinforced polymer-matrix composites (filler: E-glass or carbon fabric; matrix: epoxy or polyimide resin) were irradiated $ with^{60} $Coγ-rays or 2 MeV electrons at room temperature. Three-point bend tests were then carried out at 77 K and at room temperature in a 45° direction from warp to fill. Comparison of the degradation behaviour among these composites reveals that the glass-epoxy and glass-polyimide composites are quite similar to each other in the dose dependence of the ultimate interlaminar shear strength at each test temperature. This result suggests that the radiation damage at the fibre-matrix interface decreases the contribution of the chemical bond mode to the total bond strength at the interface, thus decreasing the composite shear strength with increasing dose. For the carbon-epoxy and carbon-polyimide composites, on the other hand, the shear strength at room temperature changes little even after irradiation up to 140 MGy, while the shear strength at 77 K decreases monotonically with increasing dose. These findings suggest that the fibre-matrix bond strength due to the friction force mode is quite insensitive to radiation, thus resulting in the dose-independent shear strength at room temperature. At 77 K, however, the friction force mode fails to function properly because of the brittleness of the matrix resin, and consequently the composite shear strength decreases with increasing dose owing to a resulting increase in the matrix brittleness. Shear Strength Bond Strength Polyimide Degradation Behaviour Matrix Resin Enthalten in Journal of materials science Kluwer Academic Publishers, 1966 25(1990), 3 vom: März, Seite 1863-1871 (DE-627)129546372 (DE-600)218324-9 (DE-576)014996774 0022-2461 nnns volume:25 year:1990 number:3 month:03 pages:1863-1871 https://doi.org/10.1007/BF01045398 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_OLC SSG-OLC-TEC GBV_ILN_11 GBV_ILN_20 GBV_ILN_23 GBV_ILN_30 GBV_ILN_32 GBV_ILN_40 GBV_ILN_62 GBV_ILN_65 GBV_ILN_70 GBV_ILN_2004 GBV_ILN_2006 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_2057 GBV_ILN_4082 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4316 GBV_ILN_4319 GBV_ILN_4323 GBV_ILN_4700 AR 25 1990 3 03 1863-1871 |
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10.1007/BF01045398 doi (DE-627)OLC2046167384 (DE-He213)BF01045398-p DE-627 ger DE-627 rakwb eng 670 VZ Egusa, S. verfasserin aut Anisotropy of radiation-induced degradation in mechanical properties of fabric-reinforced polymer-matrix composites 1990 Text txt rdacontent ohne Hilfsmittel zu benutzen n rdamedia Band nc rdacarrier © Chapman and Hall Ltd 1990 Abstract Four kinds of fabric-reinforced polymer-matrix composites (filler: E-glass or carbon fabric; matrix: epoxy or polyimide resin) were irradiated $ with^{60} $Coγ-rays or 2 MeV electrons at room temperature. Three-point bend tests were then carried out at 77 K and at room temperature in a 45° direction from warp to fill. Comparison of the degradation behaviour among these composites reveals that the glass-epoxy and glass-polyimide composites are quite similar to each other in the dose dependence of the ultimate interlaminar shear strength at each test temperature. This result suggests that the radiation damage at the fibre-matrix interface decreases the contribution of the chemical bond mode to the total bond strength at the interface, thus decreasing the composite shear strength with increasing dose. For the carbon-epoxy and carbon-polyimide composites, on the other hand, the shear strength at room temperature changes little even after irradiation up to 140 MGy, while the shear strength at 77 K decreases monotonically with increasing dose. These findings suggest that the fibre-matrix bond strength due to the friction force mode is quite insensitive to radiation, thus resulting in the dose-independent shear strength at room temperature. At 77 K, however, the friction force mode fails to function properly because of the brittleness of the matrix resin, and consequently the composite shear strength decreases with increasing dose owing to a resulting increase in the matrix brittleness. Shear Strength Bond Strength Polyimide Degradation Behaviour Matrix Resin Enthalten in Journal of materials science Kluwer Academic Publishers, 1966 25(1990), 3 vom: März, Seite 1863-1871 (DE-627)129546372 (DE-600)218324-9 (DE-576)014996774 0022-2461 nnns volume:25 year:1990 number:3 month:03 pages:1863-1871 https://doi.org/10.1007/BF01045398 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_OLC SSG-OLC-TEC GBV_ILN_11 GBV_ILN_20 GBV_ILN_23 GBV_ILN_30 GBV_ILN_32 GBV_ILN_40 GBV_ILN_62 GBV_ILN_65 GBV_ILN_70 GBV_ILN_2004 GBV_ILN_2006 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_2057 GBV_ILN_4082 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4316 GBV_ILN_4319 GBV_ILN_4323 GBV_ILN_4700 AR 25 1990 3 03 1863-1871 |
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10.1007/BF01045398 doi (DE-627)OLC2046167384 (DE-He213)BF01045398-p DE-627 ger DE-627 rakwb eng 670 VZ Egusa, S. verfasserin aut Anisotropy of radiation-induced degradation in mechanical properties of fabric-reinforced polymer-matrix composites 1990 Text txt rdacontent ohne Hilfsmittel zu benutzen n rdamedia Band nc rdacarrier © Chapman and Hall Ltd 1990 Abstract Four kinds of fabric-reinforced polymer-matrix composites (filler: E-glass or carbon fabric; matrix: epoxy or polyimide resin) were irradiated $ with^{60} $Coγ-rays or 2 MeV electrons at room temperature. Three-point bend tests were then carried out at 77 K and at room temperature in a 45° direction from warp to fill. Comparison of the degradation behaviour among these composites reveals that the glass-epoxy and glass-polyimide composites are quite similar to each other in the dose dependence of the ultimate interlaminar shear strength at each test temperature. This result suggests that the radiation damage at the fibre-matrix interface decreases the contribution of the chemical bond mode to the total bond strength at the interface, thus decreasing the composite shear strength with increasing dose. For the carbon-epoxy and carbon-polyimide composites, on the other hand, the shear strength at room temperature changes little even after irradiation up to 140 MGy, while the shear strength at 77 K decreases monotonically with increasing dose. These findings suggest that the fibre-matrix bond strength due to the friction force mode is quite insensitive to radiation, thus resulting in the dose-independent shear strength at room temperature. At 77 K, however, the friction force mode fails to function properly because of the brittleness of the matrix resin, and consequently the composite shear strength decreases with increasing dose owing to a resulting increase in the matrix brittleness. Shear Strength Bond Strength Polyimide Degradation Behaviour Matrix Resin Enthalten in Journal of materials science Kluwer Academic Publishers, 1966 25(1990), 3 vom: März, Seite 1863-1871 (DE-627)129546372 (DE-600)218324-9 (DE-576)014996774 0022-2461 nnns volume:25 year:1990 number:3 month:03 pages:1863-1871 https://doi.org/10.1007/BF01045398 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_OLC SSG-OLC-TEC GBV_ILN_11 GBV_ILN_20 GBV_ILN_23 GBV_ILN_30 GBV_ILN_32 GBV_ILN_40 GBV_ILN_62 GBV_ILN_65 GBV_ILN_70 GBV_ILN_2004 GBV_ILN_2006 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_2057 GBV_ILN_4082 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4316 GBV_ILN_4319 GBV_ILN_4323 GBV_ILN_4700 AR 25 1990 3 03 1863-1871 |
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10.1007/BF01045398 doi (DE-627)OLC2046167384 (DE-He213)BF01045398-p DE-627 ger DE-627 rakwb eng 670 VZ Egusa, S. verfasserin aut Anisotropy of radiation-induced degradation in mechanical properties of fabric-reinforced polymer-matrix composites 1990 Text txt rdacontent ohne Hilfsmittel zu benutzen n rdamedia Band nc rdacarrier © Chapman and Hall Ltd 1990 Abstract Four kinds of fabric-reinforced polymer-matrix composites (filler: E-glass or carbon fabric; matrix: epoxy or polyimide resin) were irradiated $ with^{60} $Coγ-rays or 2 MeV electrons at room temperature. Three-point bend tests were then carried out at 77 K and at room temperature in a 45° direction from warp to fill. Comparison of the degradation behaviour among these composites reveals that the glass-epoxy and glass-polyimide composites are quite similar to each other in the dose dependence of the ultimate interlaminar shear strength at each test temperature. This result suggests that the radiation damage at the fibre-matrix interface decreases the contribution of the chemical bond mode to the total bond strength at the interface, thus decreasing the composite shear strength with increasing dose. For the carbon-epoxy and carbon-polyimide composites, on the other hand, the shear strength at room temperature changes little even after irradiation up to 140 MGy, while the shear strength at 77 K decreases monotonically with increasing dose. These findings suggest that the fibre-matrix bond strength due to the friction force mode is quite insensitive to radiation, thus resulting in the dose-independent shear strength at room temperature. At 77 K, however, the friction force mode fails to function properly because of the brittleness of the matrix resin, and consequently the composite shear strength decreases with increasing dose owing to a resulting increase in the matrix brittleness. Shear Strength Bond Strength Polyimide Degradation Behaviour Matrix Resin Enthalten in Journal of materials science Kluwer Academic Publishers, 1966 25(1990), 3 vom: März, Seite 1863-1871 (DE-627)129546372 (DE-600)218324-9 (DE-576)014996774 0022-2461 nnns volume:25 year:1990 number:3 month:03 pages:1863-1871 https://doi.org/10.1007/BF01045398 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_OLC SSG-OLC-TEC GBV_ILN_11 GBV_ILN_20 GBV_ILN_23 GBV_ILN_30 GBV_ILN_32 GBV_ILN_40 GBV_ILN_62 GBV_ILN_65 GBV_ILN_70 GBV_ILN_2004 GBV_ILN_2006 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_2057 GBV_ILN_4082 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4316 GBV_ILN_4319 GBV_ILN_4323 GBV_ILN_4700 AR 25 1990 3 03 1863-1871 |
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Enthalten in Journal of materials science 25(1990), 3 vom: März, Seite 1863-1871 volume:25 year:1990 number:3 month:03 pages:1863-1871 |
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Enthalten in Journal of materials science 25(1990), 3 vom: März, Seite 1863-1871 volume:25 year:1990 number:3 month:03 pages:1863-1871 |
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Three-point bend tests were then carried out at 77 K and at room temperature in a 45° direction from warp to fill. Comparison of the degradation behaviour among these composites reveals that the glass-epoxy and glass-polyimide composites are quite similar to each other in the dose dependence of the ultimate interlaminar shear strength at each test temperature. This result suggests that the radiation damage at the fibre-matrix interface decreases the contribution of the chemical bond mode to the total bond strength at the interface, thus decreasing the composite shear strength with increasing dose. For the carbon-epoxy and carbon-polyimide composites, on the other hand, the shear strength at room temperature changes little even after irradiation up to 140 MGy, while the shear strength at 77 K decreases monotonically with increasing dose. These findings suggest that the fibre-matrix bond strength due to the friction force mode is quite insensitive to radiation, thus resulting in the dose-independent shear strength at room temperature. 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anisotropy of radiation-induced degradation in mechanical properties of fabric-reinforced polymer-matrix composites |
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Anisotropy of radiation-induced degradation in mechanical properties of fabric-reinforced polymer-matrix composites |
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Abstract Four kinds of fabric-reinforced polymer-matrix composites (filler: E-glass or carbon fabric; matrix: epoxy or polyimide resin) were irradiated $ with^{60} $Coγ-rays or 2 MeV electrons at room temperature. Three-point bend tests were then carried out at 77 K and at room temperature in a 45° direction from warp to fill. Comparison of the degradation behaviour among these composites reveals that the glass-epoxy and glass-polyimide composites are quite similar to each other in the dose dependence of the ultimate interlaminar shear strength at each test temperature. This result suggests that the radiation damage at the fibre-matrix interface decreases the contribution of the chemical bond mode to the total bond strength at the interface, thus decreasing the composite shear strength with increasing dose. For the carbon-epoxy and carbon-polyimide composites, on the other hand, the shear strength at room temperature changes little even after irradiation up to 140 MGy, while the shear strength at 77 K decreases monotonically with increasing dose. These findings suggest that the fibre-matrix bond strength due to the friction force mode is quite insensitive to radiation, thus resulting in the dose-independent shear strength at room temperature. At 77 K, however, the friction force mode fails to function properly because of the brittleness of the matrix resin, and consequently the composite shear strength decreases with increasing dose owing to a resulting increase in the matrix brittleness. © Chapman and Hall Ltd 1990 |
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Abstract Four kinds of fabric-reinforced polymer-matrix composites (filler: E-glass or carbon fabric; matrix: epoxy or polyimide resin) were irradiated $ with^{60} $Coγ-rays or 2 MeV electrons at room temperature. Three-point bend tests were then carried out at 77 K and at room temperature in a 45° direction from warp to fill. Comparison of the degradation behaviour among these composites reveals that the glass-epoxy and glass-polyimide composites are quite similar to each other in the dose dependence of the ultimate interlaminar shear strength at each test temperature. This result suggests that the radiation damage at the fibre-matrix interface decreases the contribution of the chemical bond mode to the total bond strength at the interface, thus decreasing the composite shear strength with increasing dose. For the carbon-epoxy and carbon-polyimide composites, on the other hand, the shear strength at room temperature changes little even after irradiation up to 140 MGy, while the shear strength at 77 K decreases monotonically with increasing dose. These findings suggest that the fibre-matrix bond strength due to the friction force mode is quite insensitive to radiation, thus resulting in the dose-independent shear strength at room temperature. At 77 K, however, the friction force mode fails to function properly because of the brittleness of the matrix resin, and consequently the composite shear strength decreases with increasing dose owing to a resulting increase in the matrix brittleness. © Chapman and Hall Ltd 1990 |
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Abstract Four kinds of fabric-reinforced polymer-matrix composites (filler: E-glass or carbon fabric; matrix: epoxy or polyimide resin) were irradiated $ with^{60} $Coγ-rays or 2 MeV electrons at room temperature. Three-point bend tests were then carried out at 77 K and at room temperature in a 45° direction from warp to fill. Comparison of the degradation behaviour among these composites reveals that the glass-epoxy and glass-polyimide composites are quite similar to each other in the dose dependence of the ultimate interlaminar shear strength at each test temperature. This result suggests that the radiation damage at the fibre-matrix interface decreases the contribution of the chemical bond mode to the total bond strength at the interface, thus decreasing the composite shear strength with increasing dose. For the carbon-epoxy and carbon-polyimide composites, on the other hand, the shear strength at room temperature changes little even after irradiation up to 140 MGy, while the shear strength at 77 K decreases monotonically with increasing dose. These findings suggest that the fibre-matrix bond strength due to the friction force mode is quite insensitive to radiation, thus resulting in the dose-independent shear strength at room temperature. At 77 K, however, the friction force mode fails to function properly because of the brittleness of the matrix resin, and consequently the composite shear strength decreases with increasing dose owing to a resulting increase in the matrix brittleness. © Chapman and Hall Ltd 1990 |
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