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MMPDS-01<br />

31 January 2003<br />

Maximum Stress, ksi<br />

250<br />

225<br />

200<br />

175<br />

150<br />

125<br />

100<br />

75<br />

50<br />

25<br />

+<br />

+<br />

+<br />

+<br />

+<br />

+<br />

+ +<br />

+ + +<br />

AISI 4340 RT Kt=3.0<br />

Stress Ratio<br />

-1.00<br />

0.00<br />

+ 0.54<br />

→<br />

+ →<br />

+ → →<br />

→ →<br />

→→→<br />

Runout<br />

Note: Stresses are based<br />

on net section.<br />

0<br />

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

Fatigue Life, Cycles<br />

Figure 2.3.1.3.8(o). Best-fit S/N curves for notched, K t = 3.0, AISI 4340 alloy <strong>steel</strong> bar,<br />

F tu = 260 ksi, longitudinal direction.<br />

Correlative Information for Figure 2.3.1.3.8(o)<br />

Product Form: Rolled bar, 1.125 inch diameter,<br />

air melted<br />

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

266 232 RT<br />

(unnotched)<br />

352 — RT<br />

(notched)<br />

Specimen Details: Notched, V-Groove, K t = 3.0<br />

0.270 inch gross diameter<br />

0.220 inch net diameter<br />

0.010 inch root radius, r<br />

60E flank angle, ω<br />

Surface Condition: Lathe turned to RMS 10<br />

Reference: 2.3.1.3.8(a)<br />

Test Parameters:<br />

Loading—Axial<br />

Frequency—2000 to 2500 cpm<br />

Temperature—RT<br />

Atmosphere—Air<br />

No. of Heats/Lots: 1<br />

Equivalent Stress Equation:<br />

Log N f = 7.14-1.74 log (S eq - 56.4)<br />

S eq = S max (1-R) 0.51<br />

Std. Error of Estimate, Log (Life) = 0.32<br />

Standard Deviation, Log (Life) = 0.59<br />

R 2 = 71%<br />

Sample Size = 29<br />

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

provide unrealistic life predictions for stress<br />

ratios beyond those represented above.]<br />

2-59

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