Thickness Effects on Fatigue Fracture Properties of Small Sized Materials
| Project/Area Number |
05452127
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| Research Category |
Grant-in-Aid for General Scientific Research (B)
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| Allocation Type | Single-year Grants |
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| Research Field |
Materials/Mechanics of materials
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| Research Institution | Okayama University |
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Principal Investigator |
TORII Tashiyuki Okyama University, Engineering, Professor, 工学部, 教授 (80033249)
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| Project Period (FY) |
1993 – 1994
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| Project Status |
Completed (Fiscal Year 1994)
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| Budget Amount *help |
¥5,000,000 (Direct Cost: ¥5,000,000)
Fiscal Year 1994: ¥600,000 (Direct Cost: ¥600,000)
Fiscal Year 1993: ¥4,400,000 (Direct Cost: ¥4,400,000)
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| Keywords | Film Material / Fatigue Testing Method / Fracture Mechanics / Fatigue Fracture / Grain Size / Small Sized Material / 膜疲労試験法 / 疲労き裂発生 / 疲労き裂伝ぱ / 結晶粒径 / 応力拡大係数 / き裂閉口 |
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| Research Abstract |
A new fatigue testing method was proposed by which fatigue crack propagation could be caused in a film attached to elliptical and circular holes on a base plate subjected to push-pull cyclic loads. Using a BEM and FEM,analytical results for this testing showed that the stress has not a great change due to the place in a film even though a crystallographic orientation of grain was considered, and the stress intensity factor was almost constant during the greater part of crack propagation. In the experimental results with the use of commercial-grade iron films of 100-mum thickness, the fatigue crack propagation rate was expressed by a power law of stress intensity factor range. However, a considerable residual plastic layr was left in the wake of propagation cracks on the film. In other words, effective stress intensity factor range was a good parameter controlling the fatigue crack growth in both film and bulk specimens. In addtion, using the same iron films of 100,50 and 40-mum thickness, the data of fatigue crack propagation rate under various stress amplitudes gathered together in a narrow band showing a power law of stress intensity factor range, but strictly speaking a little higher side for the thinner film. It was found that the fatigue crack propagation rate was larger under the same effective stress intensity factor range and the slip/crack initiation life was shorter for the thinner film. Also, the fatigue life was apt to decrease on the film with the smaller grain size under the same film thickness of t_f=100mum.
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Report
(3 results)
Research Products
(14 results)
