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Practical Data for Metallurgists - Timken

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ENDURANCE LIMIT, 1000 psi<br />

160<br />

140<br />

120<br />

100<br />

80<br />

60<br />

40<br />

20<br />

TENSILE STRENGTH, MPa<br />

414 552 690 828 966 1104 1241 1379 1517 1655 1793 1931<br />

EFFECTS OF SURFACE CONDITIONS AND MECHANICAL<br />

NOTCHES ON ENDURANCE OR FATIGUE LIMITS<br />

82<br />

POLISHED<br />

GROUND<br />

MACHINED<br />

HOT ROLLED,<br />

SEVERLY NOTCHED,<br />

AS FORGED<br />

60 80 100 120 140 160 180 200 220 240 260 280<br />

TENSILE STRENGTH, 1000 psi<br />

Note: Endurance limits <strong>for</strong> surfaces exposed to corrosive environment fall<br />

below the band <strong>for</strong> hot rolled, severly notched, and as <strong>for</strong>ged surfaces.<br />

CONDITIONS WHICH AFFECT<br />

FATIGUE STRENGTH<br />

The fatigue strength of a material depends on many factors of which<br />

the following are considered among the most important: (1) the<br />

strength of the material and the magnitude of the stress being applied<br />

to the material in its application, (2) the surface integrity of the material<br />

including its finish and method of manufacture, magnitude of residual<br />

stress present, and the presence of decarburization, (3) the environment<br />

in which the material is exposed in service.<br />

It must be noted that fatigue data such as that represented by the<br />

curves shown above are averages obtained from laboratory tests<br />

which approach ideal conditions and should not be considered more<br />

than a guide.<br />

F.B. Stulen and W.C. Schulte, Metals Engineering Quarterly (Am. Soc. Metals), Vol. 5,<br />

No. 3, Aug. 1965<br />

SAE Fatigue Design Handbook (AE4) - 1968<br />

Proceedings of the International Conference on Fatigue of Metals, (IME-ASME) - 1956<br />

1140<br />

966<br />

828<br />

690<br />

552<br />

414<br />

276<br />

138<br />

ENDURANCE LIMIT, MPa

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