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ssc-367 - Ship Structure Committee

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thickness effect is necessary and the ship structure plate<br />

thicknesses are not excessive, the correction factor may be<br />

neglected.<br />

The S-N curves reconanendedbyAPI for offshore platforms may be used<br />

in the computation of tubular component fatigue damage. The API X-<br />

curve and the DEn T-curve (identicalto DnV T-curve up to 10 million<br />

cycles for catholically protected areas - see Section 4.2.2)<br />

intersect at about 500,000 cycles and would yield similar lives for<br />

a plate thicknessof 1-1/4 inch (32nmI). Most tubular chord and stub<br />

thicknesses are likely to be greater than 1-1/4 inches and the<br />

applicationof correctedDEn or DnV T-curves to compute fatigue lives<br />

will result in shorter lives and considered to be appropriate.<br />

Consideringthe effectsof plate thickness,weld profile and undercut<br />

on fatigue strength and the S-N curves it may be prudent to reassess<br />

the hot spot stress range concept. Tolloczko et al (Reference 7.8)<br />

recommend modifying the definition of hot spot stress range to<br />

reflect weld toe defects. Then, the S-N curves will reflect only the<br />

size effects.<br />

7.5.2 Fatiaue DamacteComputation<br />

Fatigue lives determined based on S-N curves and Miner’s cumulative<br />

damage rule are uniformlyacceptableto certifyingand classification<br />

agencies. The national and internationalstandards allow the use of<br />

simple cumulative damage rule for the computation of damage. Large<br />

number of test results as well as the in-serviceperformance records<br />

of marine structures indicate adequacy of this approach.<br />

Alternative rules to compute fatigue damage and methods to upgrade<br />

Miner’s rule have been proposed. Although necessary to evaluate<br />

possible benefitsof such alternatives,additionalcomplexity and the<br />

cost should also be considered. Since the S-N curves are developed<br />

based on constant amplitude stress ranges, the effect of variable<br />

7-21

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