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Fatigue damage is computed as a function of orientation of the plane, and the maximum damage plane is considered as the critical plane.
The energy-based parameters PHC and VF give satisfactory life predictions when the maximum damage plane is used for the critical plane.
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In this paper, two different forms of an original multiaxial fatigue damage parameter related to the maximum fatigue damage plane are proposed for performing fatigue life prediction under various loading conditions loadings.
Under multiaxial loadings the normal strain energy density in the critical plane (i.e. the plane of the maximum damage) is understood as the energy parameter.
The planes of maximum shear strain range and maximum damage are examined as the critical plane.
In this paper, the effects of biaxial mean stress on the orientation of the critical plane defined by maximum damage under biaxial tension/compression fatigue loading conditions are investigated by analytical and computational approaches.
In the present investigation, the accuracy of two methods, i.e., the Shear Strain-Maximum Variance Method (γ-MVM) and the Maximum Damage Method (MDM), in predicting the orientation of the crack initiation planes was checked by considering several results taken from the literature and generated by testing five different metallic materials under complex multiaxial loading.
"Inflict maximum damage.
This projectile was designed to cause maximum damage.
"They are places where they can cause maximum damage".
Nor is the diabolical calculation of maximum damage surprising.
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