Fatigue crack propagaion under mixed mode loading
Abstract Mixed model fatigue crack propagation is analyzed in this paper, using a centre cracked plate geometry, loaded under uniaxial cyclic tension. Based on maximum principal stress criterion, a modified Paris expression of fatigue crack growth rate is derived in terms of ΔK and crack angle $ β_{...
Ausführliche Beschreibung
Gespeichert in:
| Autor*in: |
Gui-xin, Cao [verfasserIn] |
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| Format: |
Artikel |
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| Sprache: |
Englisch |
| Erschienen: |
1984 |
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| Schlagwörter: |
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| Anmerkung: |
© HUST Press 1984 |
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| Übergeordnetes Werk: |
Enthalten in: Ying yong shu xue he li xue / English edition - Kluwer Academic Publishers, 1980, 5(1984), 2 vom: Apr., Seite 1209-1219 |
|---|---|
| Übergeordnetes Werk: |
volume:5 ; year:1984 ; number:2 ; month:04 ; pages:1209-1219 |
| Links: |
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| DOI / URN: |
10.1007/BF01895116 |
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| Katalog-ID: |
OLC2042829641 |
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| 520 | |a Abstract Mixed model fatigue crack propagation is analyzed in this paper, using a centre cracked plate geometry, loaded under uniaxial cyclic tension. Based on maximum principal stress criterion, a modified Paris expression of fatigue crack growth rate is derived in terms of ΔK and crack angle $ β_{0} $ for an inclined crack. It is also shown that it is more convenient to express the Paris equation by means of crack lengthprojected on the x—axis, $ a_{x} $ rather than the actual length, a itself. The crack trajectory due to cyclic loading is predicted. $ β_{0} $ is varied from 29° to 90°. Experimental data on Type L3 aluminium agree fairly well with predicted values when $ β_{0} $ exceeds 30°. | ||
| 650 | 4 | |a Fatigue Crack | |
| 650 | 4 | |a Crack Growth Rate | |
| 650 | 4 | |a Fatigue Crack Growth | |
| 650 | 4 | |a Fatigue Crack Propagation | |
| 650 | 4 | |a Fatigue Crack Growth Rate | |
| 700 | 1 | |a Ding-yi, Ju |4 aut | |
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10.1007/BF01895116 doi (DE-627)OLC2042829641 (DE-He213)BF01895116-p DE-627 ger DE-627 rakwb eng 510 VZ Gui-xin, Cao verfasserin aut Fatigue crack propagaion under mixed mode loading 1984 Text txt rdacontent ohne Hilfsmittel zu benutzen n rdamedia Band nc rdacarrier © HUST Press 1984 Abstract Mixed model fatigue crack propagation is analyzed in this paper, using a centre cracked plate geometry, loaded under uniaxial cyclic tension. Based on maximum principal stress criterion, a modified Paris expression of fatigue crack growth rate is derived in terms of ΔK and crack angle $ β_{0} $ for an inclined crack. It is also shown that it is more convenient to express the Paris equation by means of crack lengthprojected on the x—axis, $ a_{x} $ rather than the actual length, a itself. The crack trajectory due to cyclic loading is predicted. $ β_{0} $ is varied from 29° to 90°. Experimental data on Type L3 aluminium agree fairly well with predicted values when $ β_{0} $ exceeds 30°. Fatigue Crack Crack Growth Rate Fatigue Crack Growth Fatigue Crack Propagation Fatigue Crack Growth Rate Ding-yi, Ju aut Enthalten in Ying yong shu xue he li xue / English edition Kluwer Academic Publishers, 1980 5(1984), 2 vom: Apr., Seite 1209-1219 (DE-627)130523747 (DE-600)770632-7 (DE-576)016095987 0253-4827 nnns volume:5 year:1984 number:2 month:04 pages:1209-1219 https://doi.org/10.1007/BF01895116 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_OLC SSG-OLC-MAT SSG-OPC-MAT GBV_ILN_11 GBV_ILN_20 GBV_ILN_40 GBV_ILN_70 GBV_ILN_2006 GBV_ILN_2088 GBV_ILN_4310 AR 5 1984 2 04 1209-1219 |
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10.1007/BF01895116 doi (DE-627)OLC2042829641 (DE-He213)BF01895116-p DE-627 ger DE-627 rakwb eng 510 VZ Gui-xin, Cao verfasserin aut Fatigue crack propagaion under mixed mode loading 1984 Text txt rdacontent ohne Hilfsmittel zu benutzen n rdamedia Band nc rdacarrier © HUST Press 1984 Abstract Mixed model fatigue crack propagation is analyzed in this paper, using a centre cracked plate geometry, loaded under uniaxial cyclic tension. Based on maximum principal stress criterion, a modified Paris expression of fatigue crack growth rate is derived in terms of ΔK and crack angle $ β_{0} $ for an inclined crack. It is also shown that it is more convenient to express the Paris equation by means of crack lengthprojected on the x—axis, $ a_{x} $ rather than the actual length, a itself. The crack trajectory due to cyclic loading is predicted. $ β_{0} $ is varied from 29° to 90°. Experimental data on Type L3 aluminium agree fairly well with predicted values when $ β_{0} $ exceeds 30°. Fatigue Crack Crack Growth Rate Fatigue Crack Growth Fatigue Crack Propagation Fatigue Crack Growth Rate Ding-yi, Ju aut Enthalten in Ying yong shu xue he li xue / English edition Kluwer Academic Publishers, 1980 5(1984), 2 vom: Apr., Seite 1209-1219 (DE-627)130523747 (DE-600)770632-7 (DE-576)016095987 0253-4827 nnns volume:5 year:1984 number:2 month:04 pages:1209-1219 https://doi.org/10.1007/BF01895116 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_OLC SSG-OLC-MAT SSG-OPC-MAT GBV_ILN_11 GBV_ILN_20 GBV_ILN_40 GBV_ILN_70 GBV_ILN_2006 GBV_ILN_2088 GBV_ILN_4310 AR 5 1984 2 04 1209-1219 |
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10.1007/BF01895116 doi (DE-627)OLC2042829641 (DE-He213)BF01895116-p DE-627 ger DE-627 rakwb eng 510 VZ Gui-xin, Cao verfasserin aut Fatigue crack propagaion under mixed mode loading 1984 Text txt rdacontent ohne Hilfsmittel zu benutzen n rdamedia Band nc rdacarrier © HUST Press 1984 Abstract Mixed model fatigue crack propagation is analyzed in this paper, using a centre cracked plate geometry, loaded under uniaxial cyclic tension. Based on maximum principal stress criterion, a modified Paris expression of fatigue crack growth rate is derived in terms of ΔK and crack angle $ β_{0} $ for an inclined crack. It is also shown that it is more convenient to express the Paris equation by means of crack lengthprojected on the x—axis, $ a_{x} $ rather than the actual length, a itself. The crack trajectory due to cyclic loading is predicted. $ β_{0} $ is varied from 29° to 90°. Experimental data on Type L3 aluminium agree fairly well with predicted values when $ β_{0} $ exceeds 30°. Fatigue Crack Crack Growth Rate Fatigue Crack Growth Fatigue Crack Propagation Fatigue Crack Growth Rate Ding-yi, Ju aut Enthalten in Ying yong shu xue he li xue / English edition Kluwer Academic Publishers, 1980 5(1984), 2 vom: Apr., Seite 1209-1219 (DE-627)130523747 (DE-600)770632-7 (DE-576)016095987 0253-4827 nnns volume:5 year:1984 number:2 month:04 pages:1209-1219 https://doi.org/10.1007/BF01895116 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_OLC SSG-OLC-MAT SSG-OPC-MAT GBV_ILN_11 GBV_ILN_20 GBV_ILN_40 GBV_ILN_70 GBV_ILN_2006 GBV_ILN_2088 GBV_ILN_4310 AR 5 1984 2 04 1209-1219 |
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10.1007/BF01895116 doi (DE-627)OLC2042829641 (DE-He213)BF01895116-p DE-627 ger DE-627 rakwb eng 510 VZ Gui-xin, Cao verfasserin aut Fatigue crack propagaion under mixed mode loading 1984 Text txt rdacontent ohne Hilfsmittel zu benutzen n rdamedia Band nc rdacarrier © HUST Press 1984 Abstract Mixed model fatigue crack propagation is analyzed in this paper, using a centre cracked plate geometry, loaded under uniaxial cyclic tension. Based on maximum principal stress criterion, a modified Paris expression of fatigue crack growth rate is derived in terms of ΔK and crack angle $ β_{0} $ for an inclined crack. It is also shown that it is more convenient to express the Paris equation by means of crack lengthprojected on the x—axis, $ a_{x} $ rather than the actual length, a itself. The crack trajectory due to cyclic loading is predicted. $ β_{0} $ is varied from 29° to 90°. Experimental data on Type L3 aluminium agree fairly well with predicted values when $ β_{0} $ exceeds 30°. Fatigue Crack Crack Growth Rate Fatigue Crack Growth Fatigue Crack Propagation Fatigue Crack Growth Rate Ding-yi, Ju aut Enthalten in Ying yong shu xue he li xue / English edition Kluwer Academic Publishers, 1980 5(1984), 2 vom: Apr., Seite 1209-1219 (DE-627)130523747 (DE-600)770632-7 (DE-576)016095987 0253-4827 nnns volume:5 year:1984 number:2 month:04 pages:1209-1219 https://doi.org/10.1007/BF01895116 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_OLC SSG-OLC-MAT SSG-OPC-MAT GBV_ILN_11 GBV_ILN_20 GBV_ILN_40 GBV_ILN_70 GBV_ILN_2006 GBV_ILN_2088 GBV_ILN_4310 AR 5 1984 2 04 1209-1219 |
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10.1007/BF01895116 doi (DE-627)OLC2042829641 (DE-He213)BF01895116-p DE-627 ger DE-627 rakwb eng 510 VZ Gui-xin, Cao verfasserin aut Fatigue crack propagaion under mixed mode loading 1984 Text txt rdacontent ohne Hilfsmittel zu benutzen n rdamedia Band nc rdacarrier © HUST Press 1984 Abstract Mixed model fatigue crack propagation is analyzed in this paper, using a centre cracked plate geometry, loaded under uniaxial cyclic tension. Based on maximum principal stress criterion, a modified Paris expression of fatigue crack growth rate is derived in terms of ΔK and crack angle $ β_{0} $ for an inclined crack. It is also shown that it is more convenient to express the Paris equation by means of crack lengthprojected on the x—axis, $ a_{x} $ rather than the actual length, a itself. The crack trajectory due to cyclic loading is predicted. $ β_{0} $ is varied from 29° to 90°. Experimental data on Type L3 aluminium agree fairly well with predicted values when $ β_{0} $ exceeds 30°. Fatigue Crack Crack Growth Rate Fatigue Crack Growth Fatigue Crack Propagation Fatigue Crack Growth Rate Ding-yi, Ju aut Enthalten in Ying yong shu xue he li xue / English edition Kluwer Academic Publishers, 1980 5(1984), 2 vom: Apr., Seite 1209-1219 (DE-627)130523747 (DE-600)770632-7 (DE-576)016095987 0253-4827 nnns volume:5 year:1984 number:2 month:04 pages:1209-1219 https://doi.org/10.1007/BF01895116 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_OLC SSG-OLC-MAT SSG-OPC-MAT GBV_ILN_11 GBV_ILN_20 GBV_ILN_40 GBV_ILN_70 GBV_ILN_2006 GBV_ILN_2088 GBV_ILN_4310 AR 5 1984 2 04 1209-1219 |
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Abstract Mixed model fatigue crack propagation is analyzed in this paper, using a centre cracked plate geometry, loaded under uniaxial cyclic tension. Based on maximum principal stress criterion, a modified Paris expression of fatigue crack growth rate is derived in terms of ΔK and crack angle $ β_{0} $ for an inclined crack. It is also shown that it is more convenient to express the Paris equation by means of crack lengthprojected on the x—axis, $ a_{x} $ rather than the actual length, a itself. The crack trajectory due to cyclic loading is predicted. $ β_{0} $ is varied from 29° to 90°. Experimental data on Type L3 aluminium agree fairly well with predicted values when $ β_{0} $ exceeds 30°. © HUST Press 1984 |
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Abstract Mixed model fatigue crack propagation is analyzed in this paper, using a centre cracked plate geometry, loaded under uniaxial cyclic tension. Based on maximum principal stress criterion, a modified Paris expression of fatigue crack growth rate is derived in terms of ΔK and crack angle $ β_{0} $ for an inclined crack. It is also shown that it is more convenient to express the Paris equation by means of crack lengthprojected on the x—axis, $ a_{x} $ rather than the actual length, a itself. The crack trajectory due to cyclic loading is predicted. $ β_{0} $ is varied from 29° to 90°. Experimental data on Type L3 aluminium agree fairly well with predicted values when $ β_{0} $ exceeds 30°. © HUST Press 1984 |
| abstract_unstemmed |
Abstract Mixed model fatigue crack propagation is analyzed in this paper, using a centre cracked plate geometry, loaded under uniaxial cyclic tension. Based on maximum principal stress criterion, a modified Paris expression of fatigue crack growth rate is derived in terms of ΔK and crack angle $ β_{0} $ for an inclined crack. It is also shown that it is more convenient to express the Paris equation by means of crack lengthprojected on the x—axis, $ a_{x} $ rather than the actual length, a itself. The crack trajectory due to cyclic loading is predicted. $ β_{0} $ is varied from 29° to 90°. Experimental data on Type L3 aluminium agree fairly well with predicted values when $ β_{0} $ exceeds 30°. © HUST Press 1984 |
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10.1007/BF01895116 |
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2024-07-03T16:52:02.570Z |
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