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.<br />

MMPDS-01<br />

31 January 2003<br />

140<br />

120<br />

4130 Sht Hard, KT=2.0 EN<br />

Mean Stress<br />

0.0<br />

50.0<br />

→<br />

Runout<br />

Maximum Stress, ksi<br />

100<br />

80<br />

60<br />

40<br />

20<br />

Note: Stresses are based<br />

on net section.<br />

→ →<br />

→<br />

→<br />

→<br />

0<br />

10 3 10 4 10 5 10 6 10 7 10 8<br />

Fatigue Life, Cycles<br />

Figure 2.3.1.2.8(g). Best-fit S/N curves for notched, K t<br />

= 2.0, 4130 alloy <strong>steel</strong><br />

sheet, F tu<br />

= 180 ksi, longitudinal direction.<br />

Correlative Information for Figure 2.3.1.2.8(g)<br />

Product Form:<br />

Sheet, 0.075 inch thick<br />

Properties: TUS, ksi TYS, ksi Temp., EF<br />

180 174 RT<br />

Specimen Details:<br />

Surface Condition:<br />

Reference:<br />

Edge Notched<br />

2.25 inches gross width<br />

1.50 inches net width<br />

0.3175 inch notch radius<br />

Electropolished<br />

3.2.3.1.8(f)<br />

Test Parameters:<br />

Loading - Axial<br />

Frequency - 21-1800 cpm<br />

Temperature - RT<br />

Environment - Air<br />

No. of Heats/Lots: Not specified<br />

Equivalent Stress Equation:<br />

Log N f = 8.87-2.81 log (S eq - 41.5)<br />

S eq = S max (1-R) 0.46<br />

Std. Error of Estimate, Log (Life) = 0.18<br />

Standard Deviation, Log (Life) = 0.77<br />

R 2 = 94%<br />

Sample Size = 19<br />

[Caution: The equivalent stress model may<br />

provide unrealistic life predictions for stress<br />

ratios beyond those represented above.]<br />

2-37

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