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ssc-367 - Ship Structure Committee

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stresses several times greater than the nominal stresses. The<br />

fatigue test results for a wide variety of shiphull stiffener<br />

geometries can be used directly with the nominal stresses.<br />

At an intersectionof a tubular brace and chord, depending on the<br />

interfacegeometry,the maximum hot-spotstressesoften occur either<br />

on the weld toe of the incoming brace member or on the main chord.<br />

The ratio of the hot-spot stress to the nominal stress is defined as<br />

the stress concentrationfactor (SCF).<br />

SCF =U.aX/Un<br />

The SCF value is probably the most important single variable that<br />

affects the fatigue life of a detail/joint,necessitating accurate<br />

determination of SCFS.<br />

There are several practical approaches for determining SCF values.<br />

The first approach is to develop an analytical model of the<br />

detail/joint and carry out a finite element analysis (FEA). When<br />

modeled correctly, determination of SCFS by FEA is a very reliable<br />

approach. The second approach is to test a physical model and<br />

obtain the hot-spot stresses from measurements. Whether a straingauged<br />

acrylicmodel or other alternativesare used, the accuracyof<br />

hot-spotstresseslargelydependson the abilityto predict hot-spot<br />

stress locations and obtain measurements in those areas.<br />

Although reliable and recommended for obtaining SCFS, these two<br />

methods are time consuming and expensive. Thus, a third approach,<br />

based on applying empirical formulations to determine SCFS, has<br />

been extensively accepted for fatigue analysis of marine<br />

structures. A set of empirical formulae developed by Kuang<br />

(Reference 3.4) were derived by evaluating extensive thin-shell<br />

finite element analyses results. The formulae proposed by Smedley<br />

(Reference 3.5) and Wordsworth (Reference3.6) of Lloyds Register<br />

were derived from evaluating the results of strain-gauged acrylic<br />

models.<br />

3-14

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