Effect of Stress Frequency on Fatigue Crack Propagation in Titanium

1982 ◽  
Vol 104 (4) ◽  
pp. 257-261 ◽  
Author(s):  
S. Takezono ◽  
M. Satoh

The effect of stress frequency on the fatigue crack propagation rate in 99.5 percent pure titanium, which has a strong strain rate dependency in the plastic region, was studied. Fatigue crack propagation tests were carried out under three stress frequencies (0.02Hz, 0.2Hz, 20Hz). An elasto/visco-plastic analysis of fatigue crack propagation was performed by the finite element method (FEM), and an analysis of the dependency of crack propagation rate on frequency and strain behavior at the crack tip. The results obtained in this study are summarized as follows: (1) It was found from the experiments that the crack propagation rate, dl/dN, was approximately in inverse proportion to fn (n>0), where f is the frequency. (2) A parameter closely related to the fatigue crack growth rate is the strain range, Δεy, or visco-plastic strain range, Δεyνp at the crack tip. (3) The effect of stress frequency on the fatigue crack propagation rate may be explained by variations of Δεy or Δεyνp based on the strain rate dependency of the material.

2008 ◽  
Vol 144 ◽  
pp. 90-93 ◽  
Author(s):  
Grzegorz Gasiak ◽  
Grzegorz Robak

The paper presents a test stand for measurements of fatigue crack propagation. The stand includes a fatigue machine MZGS–100 and a device for registration of the crack length. The test stand is equipped with a stereoscopic microscope with fluent magnification of 7× – 67.5×. The microscope can be applied for observation of fatigue crack development. The microscope is also equipped with a digital camera, which enables continuous observation of fatigue crack development on the computer monitor and it is not necessary to stop the machine. The test results obtained at this stand can be used for determination of fatigue life and fatigue crack propagation rate.


2007 ◽  
Vol 348-349 ◽  
pp. 377-380 ◽  
Author(s):  
Pavel Hutař ◽  
Luboš Náhlík ◽  
Zdeněk Knésl

The influence of corner singularity on the distribution of the stresses around the crack front for a three-dimensional structure is described in this paper. The distribution of stress singularity through the thickness of the middle tension specimen provides us an indication of crack behaviour close to a free surface. An estimation of the region where the change of singularity exponent plays an important role in fatigue crack propagation rate was carried out. A decrease in fatigue crack propagation rate close to the free surface was found. The lower fatigue crack propagation rate in the boundary layer in comparison with the interior of the specimen leads to a change of intersecting angle between crack and free surface and depends on Poisson’s ratio.


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