Fracture analysis of AA6061-graphite composite for the application of helicopter rotor blade
The main objective of the work is to study the fracture behavior of AA6061-graphite material using both experimental technique and finite element simulation by considering helicopter rotor blade as a case study. From the case study, it has been observed that the helicopter rotor blade, made of AA606...
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Language: | English |
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Gruppo Italiano Frattura
2021-10-01
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Series: | Fracture and Structural Integrity |
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Online Access: | https://www.fracturae.com/index.php/fis/article/view/3138/3333 |
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author | Saleemsab Doddamani Chao Wang M.JinnahSheik Mohamed Md. Arefin Kowser |
author_facet | Saleemsab Doddamani Chao Wang M.JinnahSheik Mohamed Md. Arefin Kowser |
author_sort | Saleemsab Doddamani |
collection | DOAJ |
description | The main objective of the work is to study the fracture behavior of AA6061-graphite material using both experimental technique and finite element simulation by considering helicopter rotor blade as a case study. From the case study, it has been observed that the helicopter rotor blade, made of AA6061, has been failed at the threaded portion of the hole. Experimental fracture toughness is carried out using the compact tension specimens as per ASTM standard testing procedure. Modeling of compact tension specimens and the threaded portion of the bolt hole was utilized to analyze the fracture toughness using a simulation tool. From the results and the comparison, it is recommended to use AA6061-9wt% graphite material as a replacement of AA6061 in the application of main rotor blades of the helicopter |
format | Article |
id | doaj-art-899f5660469143f3b6b5d2af0d61b076 |
institution | Kabale University |
issn | 1971-8993 |
language | English |
publishDate | 2021-10-01 |
publisher | Gruppo Italiano Frattura |
record_format | Article |
series | Fracture and Structural Integrity |
spelling | doaj-art-899f5660469143f3b6b5d2af0d61b0762025-01-02T23:02:23ZengGruppo Italiano FratturaFracture and Structural Integrity1971-89932021-10-01155819120110.3221/IGF-ESIS.58.1410.3221/IGF-ESIS.58.14Fracture analysis of AA6061-graphite composite for the application of helicopter rotor bladeSaleemsab DoddamaniChao WangM.JinnahSheik MohamedMd. Arefin KowserThe main objective of the work is to study the fracture behavior of AA6061-graphite material using both experimental technique and finite element simulation by considering helicopter rotor blade as a case study. From the case study, it has been observed that the helicopter rotor blade, made of AA6061, has been failed at the threaded portion of the hole. Experimental fracture toughness is carried out using the compact tension specimens as per ASTM standard testing procedure. Modeling of compact tension specimens and the threaded portion of the bolt hole was utilized to analyze the fracture toughness using a simulation tool. From the results and the comparison, it is recommended to use AA6061-9wt% graphite material as a replacement of AA6061 in the application of main rotor blades of the helicopterhttps://www.fracturae.com/index.php/fis/article/view/3138/3333metal matrix compositeal-graphite compositesimulationsfracture toughnessrotor blade |
spellingShingle | Saleemsab Doddamani Chao Wang M.JinnahSheik Mohamed Md. Arefin Kowser Fracture analysis of AA6061-graphite composite for the application of helicopter rotor blade Fracture and Structural Integrity metal matrix composite al-graphite composite simulations fracture toughness rotor blade |
title | Fracture analysis of AA6061-graphite composite for the application of helicopter rotor blade |
title_full | Fracture analysis of AA6061-graphite composite for the application of helicopter rotor blade |
title_fullStr | Fracture analysis of AA6061-graphite composite for the application of helicopter rotor blade |
title_full_unstemmed | Fracture analysis of AA6061-graphite composite for the application of helicopter rotor blade |
title_short | Fracture analysis of AA6061-graphite composite for the application of helicopter rotor blade |
title_sort | fracture analysis of aa6061 graphite composite for the application of helicopter rotor blade |
topic | metal matrix composite al-graphite composite simulations fracture toughness rotor blade |
url | https://www.fracturae.com/index.php/fis/article/view/3138/3333 |
work_keys_str_mv | AT saleemsabdoddamani fractureanalysisofaa6061graphitecompositefortheapplicationofhelicopterrotorblade AT chaowang fractureanalysisofaa6061graphitecompositefortheapplicationofhelicopterrotorblade AT mjinnahsheikmohamed fractureanalysisofaa6061graphitecompositefortheapplicationofhelicopterrotorblade AT mdarefinkowser fractureanalysisofaa6061graphitecompositefortheapplicationofhelicopterrotorblade |