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ssc-367 - Ship Structure Committee

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classified as a K joint. If the load is transferred by some<br />

combinationof shear through the joint and brace-to-brace,then the<br />

joint is classified as a KT joint.<br />

If the load is transferredthrough one side of the chord to another,<br />

then the joint is classified as an Xjoint. Figure 5-9 shows joint<br />

classification by load distribution.<br />

5.4.3<br />

Empirical Eauations<br />

Prior to the discussion of empirical equations it is beneficial to<br />

briefly discuss the available data on SCFS. Review of various<br />

publisheddata (References1.8, 5.19, 5.20, 5.21 and 5.22) indicate<br />

that substantial scatter of SCFS is observed. Variations in SCFS<br />

occur in both nominally identical joints and in symmetrical<br />

locations of joints where one would expect little variations in<br />

SCFS. Material and fabrication imperfectionscontribute to the SCF<br />

variations. Lalani et al (Reference 5.23) point out that the<br />

parameterscontributingto these variationscan be grouped intotwo:<br />

●<br />

Experimental error, including modeling, gauge position and<br />

measurements and the loading.<br />

●<br />

Expected variations due to material and fabrication<br />

imperfections,includingvariations in weld profile, size and<br />

imperfections.<br />

The use of empirical formulationshas been extensively accepted for<br />

fatigue analysisof marine structures. A set of empirical formulae<br />

developed by Kuang (Reference 3.2) were derived by evaluating<br />

extensive thin-shellFEA results. The formulae proposed by Smedley<br />

(Reference3.3) and Wordsworth (Reference3.4) of Lloyd’s Registry<br />

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

models. Other empirical equations published include those by<br />

Gibstein (References 5.21, 5.24), Efthymiou (5.19) and Wordsworth<br />

(5.25).<br />

5-29

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