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MMPDS-01<br />

31 January 2003<br />

Maximum Stress, ksi<br />

80<br />

70<br />

60<br />

50<br />

40<br />

30<br />

20<br />

10<br />

4130 Sheet Normalized, Kt=4.0,<br />

x<br />

Edge and Fillet Notches,<br />

Mean Stress =<br />

x x<br />

0.0<br />

10.0<br />

x x<br />

+ 20.0<br />

+++ ++ +<br />

x 30.0<br />

+ x x<br />

+++ +<br />

x → Runout<br />

+ + x x<br />

x x<br />

+ + x<br />

x→<br />

x→<br />

+<br />

++ + +<br />

+ →<br />

+ +<br />

+ →<br />

+++ + →<br />

+<br />

+<br />

++ →→<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(d). Best-fit S/N curves diagram for notched, K t = 4.0, 4130<br />

alloy <strong>steel</strong> sheet, normalized, longitudinal direction.<br />

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

Product Form:<br />

Sheet, 0.075 inch thick<br />

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

117 99 RT<br />

(unnotched)<br />

120 — RT<br />

(notched)<br />

K t = 4.0<br />

Specimen Details: Notched, K t = 4.0<br />

Notch Gross Net Notch<br />

Type Width Width Radius<br />

Edge 2.25 1.500 0.057<br />

Edge 4.10 1.496 0.070<br />

Fillet 2.25 1.500 0.0195<br />

Surface Condition:<br />

References:<br />

Electropolished<br />

3.2.3.1.8(b), (f), and (g)<br />

Test Parameters:<br />

Loading - Axial<br />

Frequency - 1100-1800 cpm<br />

Temperature - RT<br />

Environment - Air<br />

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

Equivalent Stress Equation:<br />

Log N f = 12.6-4.69 log (S eq )<br />

S eq = S max (1-R) 0.63<br />

Std. Error of Estimate, Log (Life) = 0.24<br />

Standard Deviation, Log (Life) = 0.70<br />

R 2 = 88%<br />

Sample Size = 87<br />

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

provide unrealistic life predictions for stress<br />

ratios beyond those represented above.]<br />

2-34

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