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As a result, the first method (MTS grips) overestimates the stretch ratio at a given stress.
The effectiveness of cracks can be determined through measuring the strain at a given stress.
For a given stress, lung strain may be completely different depending on the size of the lung.
The strain rate in Eq. (3) is determined by the deformation induced by water diffusion under a given stress.
The damage evolution under given stress and damage fields for each block loading is determined by a damage evolution equation.
If we only consider the single crystal test structure the failure happens at the same location at a fixed lifetime for a given stress condition.
A model based on experimental results has been developed which predicts weight reduction of leaf springs for a given stress at varying shot peening conditions.
Under a given stress regime, wing-cracks within a shear zone could connect consecutively in a shear zone until forming tensile fractures.
The strain at a given stress and the corresponding crack number and openings can then be obtained and the simulated stress-strain curve agrees well with experimental results.
Also, the probabilistic distribution of fatigue life of SCRC and SFRSCRC at a given stress level has been approximately modeled by the two-parameter Weibull distribution.
A general procedure and simplified direct design equations are derived taking into account equilibrium and a given stress distribution at ultimate limit states (ULS).
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CEO of Professional Science Editing for Scientists @ prosciediting.com