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Fatigue tests were performed using a stress ratio of R = 0.10.
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Fatigue tests were conducted using lap-shear specimens at a stress ratio of R = 0.1.
In this work, fatigue crack growth rate (FCGR) was evaluated in air and at room temperature under constant amplitude loading at a stress ratio of 0.1, using compact tension specimens.
A stress ratio (R) of 0.65 was used for the above mentioned stress levels.
Fatigue tests were conducted using lap-shear specimens with probe hole and re-filled one at a stress ratio of R = 0.1.
Using compact tension C(T) specimens, fatigue crack growth (FCG) tests were conducted in air under constant amplitude loading at a stress ratio of 0.5.
A stress ratio is then imposed for purposes of design.
Use a stress reliever.
Use a stress release mechanism.
When the experimental results were compared with the FEA using the stress ratio between the unmodified (completely bonded) and modified (void or disbond) cases, the results indicated that the normal stress dominates the failure behavior of the 32.2° scarf angle joint.
(a) Converting the failure criterion using stress ratio η (=τ/σ v ), the σ v -τ relation in the CNS tests becomes (b) a hyperbola.
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