Final report for WP4.3: Enhancement of design methods ... - Upwind
Final report for WP4.3: Enhancement of design methods ... - Upwind
Final report for WP4.3: Enhancement of design methods ... - Upwind
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UPWIND WP4: Offshore Support Structures and Foundations<br />
unrestrained motion (surge) [m]<br />
0.05<br />
0<br />
-0.05<br />
0 10 20 30 40 50<br />
Time [s]<br />
unrestrained motion (heave) [m]<br />
0.08<br />
0.06<br />
0.04<br />
0.02<br />
0<br />
-0.02<br />
-0.04<br />
-0.06<br />
-0.08<br />
0 10 20 30 40 50<br />
Time [s]<br />
108<br />
unrestrained motion (pitch) [deg]<br />
0.6<br />
0.4<br />
0.2<br />
0<br />
-0.2<br />
-0.4<br />
-0.6<br />
-0.8<br />
0 10 20 30 40 50<br />
Time [s]<br />
Figure 8.18: First and second-order unrestrained motions in surge, heave and pitch modes <strong>for</strong> the OC3-Hywind <strong>for</strong> a Pierson-Moskowitz<br />
spectrum with Hs=2.5 m (Tp=7.9 s).<br />
Pierson-Moskowitz spectrum with Hs=5.0 m.<br />
The comparisons <strong>of</strong> first and second-order excitation <strong>for</strong>ces in surge, heave and pitch mode <strong>for</strong> the OC3-<br />
Hywind associated with this Pierson Moskowitz spectrum (Hs=5.0 m) are shown in Figure 8.19. For this spectrum<br />
the influence <strong>of</strong> the second-order components is <strong>of</strong> the same order <strong>of</strong> magnitude as the first-order <strong>for</strong> the<br />
three modes and due to the higher frequency components the second-order excitation <strong>for</strong>ce, the total <strong>for</strong>ce<br />
shows shaper peaks when compared to the first-order excitation <strong>for</strong>ce.<br />
Excitation Force (heave) [MN]<br />
1<br />
0.5<br />
0<br />
-0.5<br />
-1<br />
0 20 40 60<br />
Time [s]<br />
80 100 120<br />
Excitation Force (surge) [MN]<br />
4<br />
3<br />
2<br />
1<br />
0<br />
-1<br />
-2<br />
-3<br />
-4<br />
0 20 40 60<br />
Time [s]<br />
80 100 120<br />
Excitation Force (pitch) [MN.m]<br />
300<br />
200<br />
100<br />
0<br />
-100<br />
-200<br />
-300<br />
0 20 40 60<br />
Time [s]<br />
80 100 120<br />
Figure 8.19: First and second-order excitation <strong>for</strong>ces in surge, heave and pitch modes <strong>of</strong> the OC3-Hywind <strong>for</strong> a Pierson-<br />
Moskowitz spectrum with Hs=5.0 m (Tp = 11.18 s).<br />
The comparisons <strong>of</strong> the first and second-order unrestrained motions <strong>of</strong> the OC3-Hywind in surge, heave and<br />
pitch associated with this spectrum are shown in Figure 8.20. The plots show a maximum amplitude value <strong>of</strong><br />
about 3m in surge, 1m in heave and 13deg in pitch. The influence <strong>of</strong> second-order unrestrained motions in<br />
surge and pitch are small, but dominant in heave when compared to the first-order motions.