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 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.
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.
public/Aluminum 1100, Su=110.0 public/Aluminum 2014-T6, Hand Forged, Su=483.0 public/Aluminum 2014-T6, Su=496.4 public/Aluminum 2014-T6, Su=510.0 public/Aluminum 2024-T3, Su=490.0 public/Aluminum 2024-T3, Su=496.4 public/Aluminum 2024-T4, Su=476.0 public/Aluminum 2024-T6, Su=475.8 public/Aluminum 5083-0, BHN=93 public/Aluminum 5083-H12, Su=385.0 public/Aluminum 5183-0, Weld metal, BHN=92 public/Aluminum 5454, Forged, Su=334.0 public/Aluminum 5456-H311, Su=400.0 public/Aluminum 6061-T6, Forged, Su=389.0 public/Aluminum 6061-T6, Hand Forged, Su=340.0 public/Aluminum 6061-T6, Sheet, Su=314.0 public/Aluminum 6061-T6, Su=310.3 public/Aluminum 7049-T73, Su=517.1 public/Aluminum 7049-T73, Su=537.8 public/Aluminum 7050-T7351X, Su=517.1 public/Aluminum 7050-T7451 plate, Su=530.9 public/Aluminum 7050-T7451 plate, Su=544.7 public/Aluminum 7050-T7452, Su=524.0 public/Aluminum 7050-T7452, Su=537.8 public/Aluminum 7050-T7651X, Su=599.9 public/Aluminum 7075-T6, Su=565.4 public/Aluminum 7075-T6, Su=572.0 public/Aluminum 7075-T6, Su=579.0 public/Aluminum 7075-T651, Su=580.0 public/Aluminum 7149-T73, Su=503.3 public/Aluminum 7175-T73, Hand Forged, Su=524.0 public/Aluminum 7175-T73611, Su=524.0 public/Aluminum 7175-T74, Su=510.2 public/Aluminum 7475-T7351 plate, Su=482.6 public/Aluminum A356-T6, Cast, Su=252.0 public/Aluminum A356-T6, Cast, Su=266.0 public/Aluminum A356-T6, Cast, Su=283.0 public/Nickel IN-718, Su=1420.0 public/Stainless Steel 30304, Cold Rolled, BHN=327 public/Stainless Steel 30304, Hot Rolled, BHN=160 public/Stainless Steel 30304, Su=650.0 public/Stainless Steel 30310, Hot Rolled, BHN=145 public/Steel 1005, HR Sheet, Su=359.0 public/Steel 1008, HR Sheet, Su=363.0 public/Steel 1015, Normalized, Su=414.0 public/Steel 1018, BHN=120 public/Steel 1020, BHN=120 public/Steel 1020, HR Plate, BHN=108 public/Steel 1020, Su=455.0 public/Steel 1040, Cold Drawn, BHN=225 public/Steel 1045, Annealed, BHN=225 public/Steel 1045, Normalized, BHN=153 public/Steel 1045, Q&T, BHN=277 public/Steel 1045, Q&T, BHN=336 public/Steel 1045, Q&T, BHN=390 public/Steel 1045, Q&T, BHN=410 public/Steel 1045, Q&T, BHN=500 public/Steel 1045, Q&T, BHN=563 public/Steel 1045, Q&T, BHN=595 public/Steel 300M, Su=1958.2 public/Steel 4130 sheet, Su=1241.1 public/Steel 4130 sheet, Su=806.7 public/Steel 4130, BHN=259 public/Steel 4130, Q&T, BHN=366 public/Steel 4140, Q&T, BHN=293 public/Steel 4140, Q&T, BHN=475 public/Steel 4142, As Quenched, BHN=670 public/Steel 4142, Q&T, BHN=380 public/Steel 4142, Q&T, BHN=400 public/Steel 4142, Q&T, BHN=450 public/Steel 4142, Q&T, BHN=450 public/Steel 4142, Q&T, BHN=475 public/Steel 4340 bar, Su=1089.4 public/Steel 4340 bar, Su=1482.4 public/Steel 4340 bar, Su=1896.1 public/Steel 4340 bar, Su=861.9 public/Steel 4340, Hot Rolled, BHN=243 public/Steel 4340, Q&T, BHN=275 public/Steel 4340, Q&T, BHN=409 public/Steel 4340, Su=1172.0 public/Steel 5160, Q&T, BHN=430 public/Steel 8620H, Case, Su=1600.0 public/Steel 8620H, Core, Su=1510.0 public/Steel 8630, Cast, BHN=254 public/Steel 9262, BHN=260 public/Steel 9262, BHN=275 public/Steel 9262, BHN=405 public/Steel A-517 Grade F, BHN=256 public/Steel A27, Cast, BHN=135 public/Steel A36, BHN=160 public/Steel A36, HAZ, BHN=243 public/Steel A36, Su=540.0 public/Steel A514, BHN=303 public/Steel A514, HAZ, BHN=461 public/Steel E110-WM(1P), Weld Metal, BHN=362 public/Steel E110-WM(2P), Weld Metal, BHN=310 public/Steel E60S-3-WM(1P), Weld Metal, BHN=233 public/Steel E60S-3-WM(2P), Weld Metal, BHN=201 public/Steel H1000 bar, Su=1413.5 public/Steel H1000, Su=1447.9 public/Steel H1050 sheet, Su=1385.9 public/Steel H900 bar, Su=1392.8 public/Steel H950 bar, Su=1689.3 public/Steel HY130, Su=1103.0 public/Steel IN787, BHN=188 public/Steel ManTen, Su=565.0 public/Steel RQC-100, Su=863.0 public/Steel TH1050 sheet, Su=1206.6 public/Steel TH1050 sheet, Su=1385.9 public/Steel-Maraging 18Ni(250), BHN=500
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.
The type of loading, axial, bending, or torsion has an effect because of the stress gradient in bending and torsion.
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.
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.
Either specify Kf directly or enter Kt and the radius.