Probabilistic Stress-Life Analysis

If needed, please go to the Constant Amplitude section for a review of the general terms and terminology related to Stress-Life fatigue analysis.

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Description of Distribution Types

Loading

Loading on structures frequently follows a Normal or LogNormal distribution. In a well controlled situation, such as may be encountered in a test track or in an electric motor, the coefficient of variation COV is typically 0.1. The COV increases to as much as 0.5 for uncontrolled customer usage. In the absence of any other information, a reasonable value of 0.2 or 0.3 may be assumed. If you enter a value of zero for either the normal or the uniform distribution types, you should enter the standard deviation for the scale parameter. This allows you to generate a distribution around zero.

Loading Units  
        Distribution Type Scale Parameter
Maximum   Smax or emax =  
Minimum   Smin or emin =  
OR
Alternating   Sa or ea =  
Mean   Sm or em =  

Material

Material properties are the most common source of uncertainty in a fatigue life calculation. Fatigue is a weakest link process and fatigue cracks start from the most severe flaw in the material. There is considerable variability in fatigue lives often a factor of 2 - 10 in fatigue life. But because of the strong dependance of fatigue life on stress or strength, the COV of material properties is on the order of 0.1 - 0.2.

You may load a material from the database by selecting it and clicking on "Load Material", or browse the database by clicking the "Material Property Finder" button, or specify individual properties directly. Clicking "Material Property Estimator" will show the default properties that are computed from the input values.

For registered users, the Material Property Estimator will display a curve plot. Registered users may also save this material in their personal database by clicking the "Save Material" button.

Name
Type
        Distribution Type Scale Parameter Correlation Coefficient
Ultimate Strength Su =  
Elastic Modulus   E =  
Fatigue Limit   SFL =
Fatigue Limit Cycles   NFL = Cycles      
Intercept   Sf′ =
Slope   b =  

Modifying Factors

The various modifying factors sometimes play an important role in calculating the fatigue life. A normal distribution is typically used with a coefficient of variation, COV, of 0.1 as a reasonable value.

        Distribution Type Scale Parameter
Surface Factor kSF = or

The type of loading, axial, bending, or torsion has an effect because of the stress gradient in bending and torsion.

           
Loading Factor kL = or  

Fatigue is controlled by the weakest link. Small parts have a larger fatigue strength than larger ones because there is a higher volume of highly stressed material. The size affect may be correlated to the volume of the material subjected to 95% of the maximum stress. It is computed from the diameter of the part. An effective diameter is used for non-circular sections. The effective part diameter may be visualized as modeling the stress gradient as a simple bending beam with the effective diameter.

Either specify ksize directly or enter the diameter.

           
Size Factor   ksize =  
Diameter d =  

Stress Concentration Factor

The stress concentration factor, Kt, is subject to any uncertainties in the model used to obtain its value as well as any variability in the structure. A normal distribution is typically used with a coefficient of variation, between 0.05 and 0.3.

        Distribution Type Scale Parameter
Stress Concentration Factor Kt =  

Either specify Kf directly or enter Kt and the radius.

           
Use Kf in analysis?  
Fatigue Notch Factor   Kf =  
Radius r =  

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