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another energy component which is added to the A15-contribution representing direct heeling<br />

moments introduced by beam wave components (Aext). Then the mean, speed independent,<br />

limiting wave height is calculated by:<br />

A0<br />

{ ( ) = 0}<br />

!<br />

H H | A A + A<br />

H := ∈ −<br />

[10]<br />

40min<br />

15diff<br />

To account for the dependency between limiting wave height and the encounter frequency<br />

the function f is determined by regression from simulated results. For this purpose the mean<br />

limiting wave height from the simulations over all speeds is calculated. Then, the difference<br />

between the actual limiting wave height at a certain speed and the mean value is determined.<br />

Fig. 10 shows the results for all cases in our database. Although the results are scattered<br />

significantly the 1:1 and 2:1 resonance conditions are clearly imprinted in the data set. The<br />

regression function, shown in Fig. 10 as green curve is calculated with the following<br />

approach:<br />

f 0 ( ωe<br />

/ ωs<br />

, Ci<br />

)<br />

( 2.8, C ) + C ω<br />

⎧<br />

f ( ωe<br />

/ ωs<br />

, Ci<br />

) = ⎨<br />

⎩ f 0 i 9 ⋅<br />

for<br />

e / ωs<br />

ωe<br />

/ ωs<br />

< 2.8<br />

for ωe<br />

/ ωs<br />

≥ 2.8<br />

[11]<br />

The function f0 is a combination of three sine-functions and reads as follows:<br />

f<br />

0<br />

Fig. 10: Frequency dependency of the limiting wave<br />

( ωe<br />

/ ωs<br />

, Ci<br />

) = C1<br />

⋅ sin(<br />

2πωe<br />

/ ωs<br />

− C2<br />

⋅ π / 2)<br />

C3<br />

⋅ sin(<br />

πωe<br />

/ ωs<br />

− C4<br />

⋅ π / 2)<br />

C5<br />

⋅ sin(<br />

C6πωe<br />

/ ωs<br />

− C7<br />

⋅ π / 2)<br />

+ C8<br />

The regression coefficients C1 through C11 are determined at the following values:<br />

ext<br />

[12]<br />

43

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