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ssc-367 - Ship Structure Committee

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The finite element models of increasing mesh refinement are often<br />

used to obtain accurate stress range data locally in fatigue<br />

sensitive areas. Thus, an overall coarse mesh model of the<br />

structure used in the first stage of analyses is modified by<br />

increasingmesh refinement in various fatigue sensitive areas. The<br />

finite element models are typically built from membrane plate<br />

elements,bendingplate elements,bar elementsand beam elementsand<br />

further discussed in Section 5.<br />

Because the individual joints and members define the global<br />

structure, the boundary conditions should also reflect the true<br />

response of the structure when subjected to the excitation<br />

loads. For a bottom-supported structure, individual piles can be<br />

simulated by individual springs. Whatever the support<br />

characteristics,a foundationmatrix can be developed to represent<br />

the foundation-structureinterface at the seafloor. It should be<br />

noted that the foundation matrix developed for an extreme<br />

environmentwould be too flexible for a milder fatigue environment.<br />

Thus, the foundationmatrix developed should be compatiblewith the<br />

applicable load range.<br />

Stress Response Amplitude Operators (RAOS)<br />

The stress RAOS or stress transfer functions are obtained by<br />

unitizing the stress ranges. If the wave height specified is other<br />

than the unit wave height (doubleamplitude of 2 feet or 2 meters),<br />

stress ranges at each frequency are divided by the wave heights<br />

input to generate the loads. Similarly, wind loads computed based<br />

on cyclic wind velocities at each frequency are divided by the<br />

respective velocities to obtain the unitized stress ranges.<br />

Stress Concentration Factors [SCF] and Hot Spot Stresses<br />

The stresses obtained from a stiffness analysis, and the RAOS<br />

generated,representnominalor averagestresses. However,the load<br />

path and the detailing of orthotropically stiffened plate or an<br />

intersection of tubular members will exhibit hot-spot or peak<br />

3’13<br />

/ Ii7<br />

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