Experimental and Numerical Modeling of the Stress Rupture Behavior of Nickel-Based Single Crystal Superalloys Subject to Multi-Row Film Cooling Holes
The stress rupture behavior of nickel-base single crystal superalloys is a primary issue facing aero-engine design, which has been studied for more than 40 years. To a large degree, it is the existence of film cooling holes with the introduction of air cooling techniques that adds the extra challeng...
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Published in | Metals (Basel ) Vol. 7; no. 9; p. 340 |
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Abstract | The stress rupture behavior of nickel-base single crystal superalloys is a primary issue facing aero-engine design, which has been studied for more than 40 years. To a large degree, it is the existence of film cooling holes with the introduction of air cooling techniques that adds the extra challenge to the problem. Using both experimental and numerical methods, we explore here the stress rupture behavior of nickel base single crystal plate specimens subject to multi-row film cooling holes. As the numerical simulation part, finite element analysis using Abaqus was performed. Numerical results reveal that the existence of film-holes causes stress concentration and transforms local stress from uniaxial to multi-axial. For the stress distribution of different types of specimens, we defined a stress multiaxiality factor to quantitatively characterize the degree of the stress complexity and examined its effect on the rupture behaviors of the specimens along with the true stress concentration factor. The test was also carried out and results indicated that the creep rupture lives of one- and two-row specimens turn out to be longer than those of non-hole specimen. However, the three- and four-row configuration showed the opposite trend. Among the geometric parameters of film-hole configuration, film-hole row spacing is a predominant one influencing the creep rupture properties. Numerical results agree well with the fracture positions and shapes of specimens. |
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AbstractList | The stress rupture behavior of nickel-base single crystal superalloys is a primary issue facing aero-engine design, which has been studied for more than 40 years. To a large degree, it is the existence of film cooling holes with the introduction of air cooling techniques that adds the extra challenge to the problem. Using both experimental and numerical methods, we explore here the stress rupture behavior of nickel base single crystal plate specimens subject to multi-row film cooling holes. As the numerical simulation part, finite element analysis using Abaqus was performed. Numerical results reveal that the existence of film-holes causes stress concentration and transforms local stress from uniaxial to multi-axial. For the stress distribution of different types of specimens, we defined a stress multiaxiality factor to quantitatively characterize the degree of the stress complexity and examined its effect on the rupture behaviors of the specimens along with the true stress concentration factor. The test was also carried out and results indicated that the creep rupture lives of one- and two-row specimens turn out to be longer than those of non-hole specimen. However, the three- and four-row configuration showed the opposite trend. Among the geometric parameters of film-hole configuration, film-hole row spacing is a predominant one influencing the creep rupture properties. Numerical results agree well with the fracture positions and shapes of specimens. |
Author | Liu, Xinling Xu, Yuanming Zhang, Weifang Sun, Weikang Dai, Wei Hu, Chunyan |
Author_xml | – sequence: 1 givenname: Yuanming surname: Xu fullname: Xu, Yuanming – sequence: 2 givenname: Weikang surname: Sun fullname: Sun, Weikang – sequence: 3 givenname: Wei orcidid: 0000-0002-7376-6977 surname: Dai fullname: Dai, Wei – sequence: 4 givenname: Chunyan surname: Hu fullname: Hu, Chunyan – sequence: 5 givenname: Xinling surname: Liu fullname: Liu, Xinling – sequence: 6 givenname: Weifang surname: Zhang fullname: Zhang, Weifang |
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CitedBy_id | crossref_primary_10_1016_j_jmrt_2024_02_040 crossref_primary_10_1016_j_engfracmech_2024_110749 crossref_primary_10_3390_met8121055 crossref_primary_10_1016_j_jallcom_2018_12_232 crossref_primary_10_1016_j_jallcom_2019_04_139 crossref_primary_10_1016_j_energy_2023_127774 crossref_primary_10_3390_en16020937 crossref_primary_10_3390_met8040233 crossref_primary_10_3390_met8080632 crossref_primary_10_1007_s11665_022_07618_2 crossref_primary_10_1016_j_jallcom_2019_05_143 |
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SubjectTerms | Air cooling Axial stress Computer simulation Cooling creep rupture behavior Crystals Engine design FEA Film cooling Finite element method flim cooling hole Mathematical models Nickel base alloys Numerical methods Rupture single crystal Single crystals Stress concentration Stress distribution superalloy Superalloys True stress |
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Title | Experimental and Numerical Modeling of the Stress Rupture Behavior of Nickel-Based Single Crystal Superalloys Subject to Multi-Row Film Cooling Holes |
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