STUDY OF FATIGUE CRACK GROWTH IN 6063-T6 ALUMINUM ALLOY
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| Format: | Artículo científico |
| Langue: | en |
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Instituto Federal de Educação, Ciência e Tecnologia de São Paulo
2015
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| _version_ | 1876459949782990848 |
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| author | Nirpesh Vikram |
| author_facet | Nirpesh Vikram |
| contents | STUDY OF FATIGUE CRACK GROWTH IN 6063-T6 ALUMINUM ALLOY Nirpesh Vikram Raghuvir Kumar Administración y Contabilidad 6063 Fatigue Fracture T6 Al Alloy Crack Closure The present study relates to in vestigate the crack propagation behavior of 6063 T6 Al Aluminum A lloy under fatigue loading. Th e experimental as well as analytica l analysis was done and for cr ack growth rate for 6063-T6 Aluminum Alloy. All analysis was done o n Side edge notch specimen. A program was developed on Matlab® t o calculate crack growth rate and effective stress intensity rang e ratio based on polynomial algorithm. That gave a very good agreement between them. The effective stress intensity range ratio (U) wa s found to depend on stress ratio (R). Variation in load range affects the crack growth rate. For constant load range its variation was negligib le, constant C was almost constant a t variable load range. Variatio n of maximum load affects constant C. 2015 artículo científico 2236-269X https://www.redalyc.org/articulo.oa?id=449544332009 en http://www.redalyc.org/revista.oa?id=4495 Independent Journal of Management & Production application/pdf Instituto Federal de Educação, Ciência e Tecnologia de São Paulo Independent Journal of Management & Production (Brasil) Num.4 Vol.6 |
| format | Artículo científico |
| id | redalyc_449544332009 |
| institution | Redalyc |
| language | en |
| publishDate | 2015 |
| publisher | Instituto Federal de Educação, Ciência e Tecnologia de São Paulo |
| spellingShingle | STUDY OF FATIGUE CRACK GROWTH IN 6063-T6 ALUMINUM ALLOY Nirpesh Vikram Administración y Contabilidad 6063 Fatigue Fracture T6 Al Alloy Crack Closure STUDY OF FATIGUE CRACK GROWTH IN 6063-T6 ALUMINUM ALLOY Nirpesh Vikram Raghuvir Kumar Administración y Contabilidad 6063 Fatigue Fracture T6 Al Alloy Crack Closure The present study relates to in vestigate the crack propagation behavior of 6063 T6 Al Aluminum A lloy under fatigue loading. Th e experimental as well as analytica l analysis was done and for cr ack growth rate for 6063-T6 Aluminum Alloy. All analysis was done o n Side edge notch specimen. A program was developed on Matlab® t o calculate crack growth rate and effective stress intensity rang e ratio based on polynomial algorithm. That gave a very good agreement between them. The effective stress intensity range ratio (U) wa s found to depend on stress ratio (R). Variation in load range affects the crack growth rate. For constant load range its variation was negligib le, constant C was almost constant a t variable load range. Variatio n of maximum load affects constant C. 2015 artículo científico 2236-269X https://www.redalyc.org/articulo.oa?id=449544332009 en http://www.redalyc.org/revista.oa?id=4495 Independent Journal of Management & Production application/pdf Instituto Federal de Educação, Ciência e Tecnologia de São Paulo Independent Journal of Management & Production (Brasil) Num.4 Vol.6 |
| title | STUDY OF FATIGUE CRACK GROWTH IN 6063-T6 ALUMINUM ALLOY |
| topic | Administración y Contabilidad 6063 Fatigue Fracture T6 Al Alloy Crack Closure |
| url | https://www.redalyc.org/articulo.oa?id=449544332009 |