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The strain distribution contours and the maximum total principal strains of the rubber mount at different loads in the x and y directions were obtained using finite element analysis method.
Then the maximum total principal strain was used as the fatigue parameter, which was substituted into the natural rubber's fatigue life equation, to predict the fatigue life of the rubber mount.
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Because there were nominal, ordinal and continuous variables, the PRINQUAL (principal components of qualitative data) procedure with maximum total variance method was used to obtain the correlation matrix.
The maximum total score possible is 40.
The possible maximum total score is 30.
Maximum total score is one hundred.
The maximum total score was 16 points.
The maximum total score is 28.
The results show that when the fiber volume fraction of the 3D five-directional braided preform is given, the equivalent stress of the composite joint decreases monotonically as the braiding angle increases, while the normal stress, maximum principal stress and total deformation firstly decreases and then increases.
Different failure criteria can be introduced with this keyword based on maximum principal strain, maximum shear strain, pressure, principal stress, and damage.
However, these observations are not incorporated in the classical fatigue life predictors for rubber, i.e. the maximum principal stretch, the maximum principal stress and the strain energy.
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