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Assessment of Crack Growth and Fatigue Life of an Axial Fan Blade Based on a Co-Simulation Approach
This paper presents static and dynamic stress analyses of an axial fan blade, which were carried out under real-life centrifugal and aerodynamic loading conditions using the Abaqus software. The location of the crack was identified on the pressure side of the blade at the conjunction between the bla...
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Published in: | Advances in materials science 2023-09, Vol.23 (3), p.61-79 |
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description | This paper presents static and dynamic stress analyses of an axial fan blade, which were carried out under real-life centrifugal and aerodynamic loading conditions using the Abaqus software. The location of the crack was identified on the pressure side of the blade at the conjunction between the blade and the blade root. It reveals a high agreement between the predicted location of stress distribution and the real origin of the crack location. Furthermore, a fracture mechanics criterion was adopted to simulate fatigue crack growth. This was performed using a fracture analysis FRANC3D code for three-dimensional problems. As a result, the calculated stress intensity factors (SIFs) were presented for the first steps, and the fatigue life of the fan blade was evaluated using the Forman de Koning model at different stress ratios. |
doi_str_mv | 10.2478/adms-2023-0017 |
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The location of the crack was identified on the pressure side of the blade at the conjunction between the blade and the blade root. It reveals a high agreement between the predicted location of stress distribution and the real origin of the crack location. Furthermore, a fracture mechanics criterion was adopted to simulate fatigue crack growth. This was performed using a fracture analysis FRANC3D code for three-dimensional problems. As a result, the calculated stress intensity factors (SIFs) were presented for the first steps, and the fatigue life of the fan blade was evaluated using the Forman de Koning model at different stress ratios.</description><identifier>ISSN: 2083-4799</identifier><identifier>ISSN: 1730-2439</identifier><identifier>EISSN: 2083-4799</identifier><identifier>DOI: 10.2478/adms-2023-0017</identifier><language>eng</language><publisher>Gdansk: Sciendo</publisher><subject>Aerodynamic loads ; Axial stress ; Axial-fan-blade ; Crack propagation ; Fatigue crack growth ; Fatigue failure ; Fatigue life ; Fatigue life assessment ; Finite element method ; Fracture mechanics ; Investigations ; Materials fatigue ; Materials science ; Mining industry ; Ratios ; Simulation ; Stress analysis ; Stress concentration ; Stress distribution ; Stress intensity factors ; Stress ratios ; Ventilation</subject><ispartof>Advances in materials science, 2023-09, Vol.23 (3), p.61-79</ispartof><rights>2023. 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As a result, the calculated stress intensity factors (SIFs) were presented for the first steps, and the fatigue life of the fan blade was evaluated using the Forman de Koning model at different stress ratios.</description><subject>Aerodynamic loads</subject><subject>Axial stress</subject><subject>Axial-fan-blade</subject><subject>Crack propagation</subject><subject>Fatigue crack growth</subject><subject>Fatigue failure</subject><subject>Fatigue life</subject><subject>Fatigue life assessment</subject><subject>Finite element method</subject><subject>Fracture mechanics</subject><subject>Investigations</subject><subject>Materials fatigue</subject><subject>Materials science</subject><subject>Mining industry</subject><subject>Ratios</subject><subject>Simulation</subject><subject>Stress analysis</subject><subject>Stress concentration</subject><subject>Stress distribution</subject><subject>Stress intensity factors</subject><subject>Stress ratios</subject><subject>Ventilation</subject><issn>2083-4799</issn><issn>1730-2439</issn><issn>2083-4799</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2023</creationdate><recordtype>article</recordtype><sourceid>PIMPY</sourceid><recordid>eNptkL1PwzAQxS0EEqWwMltiTvFHHNtiSiNakCoxALPlOnabko9iJyr973FUJBiY7k53773TD4BbjGYk5eJel01ICCI0QQjzMzAhSNAk5VKe_-kvwVUIO4QySjidAJOHYENobNvDzsHCa_MBl7479Fuo2xIudF9tBgtXlbPjgW5h_lXpOi5aOK91aeFcB1vCroUaFl3yWjVDHUVxzvd732mzvQYXTtfB3vzUKXhfPL4VT8nqZflc5KvEECH7hKR0bVJTSsyoZKnAksY3hWAMccM5ztBaU26MpYaWjlnGHaKIO8NcxjjCdAruTr4x9nOwoVe7bvBtjFREZGkmMxHpTMHsdGV8F4K3Tu191Wh_VBipEaQaQaoRpBpBRsHDSXDQdW99aTd-OMbm1_1_IaE0w_Qb6Kp3xA</recordid><startdate>20230901</startdate><enddate>20230901</enddate><creator>Hassen, Mariem Ben</creator><creator>Fakhari, Seyyed Mojtaba</creator><creator>Mrad, Hatem</creator><general>Sciendo</general><general>De Gruyter Poland</general><scope>AAYXX</scope><scope>CITATION</scope><scope>7SR</scope><scope>8BQ</scope><scope>8FD</scope><scope>8FE</scope><scope>8FG</scope><scope>ABJCF</scope><scope>ABUWG</scope><scope>AFKRA</scope><scope>AZQEC</scope><scope>BENPR</scope><scope>BGLVJ</scope><scope>BYOGL</scope><scope>CCPQU</scope><scope>D1I</scope><scope>DWQXO</scope><scope>HCIFZ</scope><scope>JG9</scope><scope>KB.</scope><scope>PDBOC</scope><scope>PIMPY</scope><scope>PQEST</scope><scope>PQQKQ</scope><scope>PQUKI</scope><scope>PRINS</scope></search><sort><creationdate>20230901</creationdate><title>Assessment of Crack Growth and Fatigue Life of an Axial Fan Blade Based on a Co-Simulation Approach</title><author>Hassen, Mariem Ben ; 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The location of the crack was identified on the pressure side of the blade at the conjunction between the blade and the blade root. It reveals a high agreement between the predicted location of stress distribution and the real origin of the crack location. Furthermore, a fracture mechanics criterion was adopted to simulate fatigue crack growth. This was performed using a fracture analysis FRANC3D code for three-dimensional problems. As a result, the calculated stress intensity factors (SIFs) were presented for the first steps, and the fatigue life of the fan blade was evaluated using the Forman de Koning model at different stress ratios.</abstract><cop>Gdansk</cop><pub>Sciendo</pub><doi>10.2478/adms-2023-0017</doi><tpages>19</tpages><oa>free_for_read</oa></addata></record> |
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subjects | Aerodynamic loads Axial stress Axial-fan-blade Crack propagation Fatigue crack growth Fatigue failure Fatigue life Fatigue life assessment Finite element method Fracture mechanics Investigations Materials fatigue Materials science Mining industry Ratios Simulation Stress analysis Stress concentration Stress distribution Stress intensity factors Stress ratios Ventilation |
title | Assessment of Crack Growth and Fatigue Life of an Axial Fan Blade Based on a Co-Simulation Approach |
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