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ssc-367 - Ship Structure Committee

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typically from 0.6 to 0.8 and 1.5 to 2.0, respectively. Very<br />

comprehensive experimental data obtained from full-scale<br />

measurements of the second Christchurch Bay Tower (References5.9,<br />

5.10 and 5.11) validate the coefficients in use today. As<br />

illustrated on Figure 5-3, the Cd and the Cm values applicable for<br />

most cylindrical members near the water surface (Level 3) are 0.66<br />

and 1.8, respectively. Although these values are applicable for<br />

Keulegan-Carpenter (Ke) number in excess of 30, even when Ke is<br />

reduced to 5, the inertiacoefficient,Cm, value reaches 2.0, while<br />

the drag coefficient, Cd, gradually increases to unity at Ke equal<br />

to 10.<br />

These coefficients also decrease with the distance from the water<br />

surface. However,becausethe uncertaintiesinmarine growth (which<br />

directly affects the surface roughness and therefore the drag<br />

coefficient)and the additionaleffortnecessaryto input,check and<br />

justify different coefficients,it is advisableto use one set ofC~<br />

and Cm values.<br />

The use of conventionalMorison’s equation and the wave kinematics<br />

for regular two-dimensionalwaves has proven to be valid for jacket<br />

structures in moderate water depths. Assessment of measureclwave<br />

forcedata (Reference5.12) for extremewave loading associatedwith<br />

directionally spread seas in a hurricaneenvironment in the Gulfof<br />

Mexico compares quite well with those analytically computed.<br />

Morison’s equation is<br />

cylindrical members by<br />

also valid to compute forces on nonapplying<br />

appropriate Cd and Cm values and<br />

equivalent diameters. Suitable values of Cd and Cm for different<br />

cross-sections may be obtained from a Det norske Veritas (DnV)<br />

document (Reference4.16.)<br />

If the extreme loadings are to be computed, an applicable wave<br />

theory, compatiblewith the wave steepness,water depth, etc., must<br />

be used. The applied total load on a structure composed of many<br />

members is then the cumulative sum of loads computed on each member<br />

5-18

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