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Final report for WP4.3: Enhancement of design methods ... - Upwind

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UPWIND WP4: Offshore Support Structures and Foundations<br />

The commercial s<strong>of</strong>tware WAMIT (v6.1s) was used to compute both the linear and weakly nonlinear hydrodynamic<br />

loads and unrestrained motions <strong>for</strong> the two structures considered in this study. This s<strong>of</strong>tware solves the<br />

hydrodynamic problem in the frequency domain. The generalisation <strong>of</strong> the second order theory to the case <strong>of</strong><br />

wave-body interactions with irregular waves requires the definition <strong>of</strong> bi-chromatic wave components and the<br />

solution is obtained in terms <strong>of</strong> the sum- and difference- frequency components <strong>of</strong> the usual hydrodynamic<br />

quantities. The second order excitation <strong>for</strong>ces are obtained as the sum <strong>of</strong> the <strong>for</strong>ce quadratic transfer functions<br />

(QTF) in the sum- and difference-frequency.<br />

The linear and weakly nonlinear comparison exercise is focused on the excitation <strong>for</strong>ces and unrestrained motions<br />

associated with regular waves and irregular waves which interact with the two <strong>of</strong>fshore wind structures.<br />

For a monochromatic wave the second order excitation <strong>for</strong>ce can be expressed as the sum <strong>of</strong> only two components<br />

<strong>of</strong> the <strong>for</strong>ce QTF in the double and zero frequency. For the OC3-Hywind the second order excitation <strong>for</strong>ce<br />

associated with the three monochromatic waves studied is much smaller than the first order excitation <strong>for</strong>ce<br />

component in all modes <strong>of</strong> motion. For the semi-submersible plat<strong>for</strong>m the second order component <strong>of</strong> the excitation<br />

<strong>for</strong>ce is dominant over the first order component <strong>for</strong> the less steep wave (period 5s) <strong>for</strong> all modes except<br />

heave. The importance <strong>of</strong> the second order component decreases <strong>for</strong> the steeper waves being smaller than the<br />

first order <strong>for</strong> the steepest wave (with period equal to 9s).<br />

The unrestrained motions <strong>of</strong> the two structures <strong>for</strong> the three monochromatic waves studied in this <strong>report</strong> are<br />

small. For the OC3-Hywind, the second-order component <strong>of</strong> the excitation <strong>for</strong>ce is negligible when compared<br />

with the first order <strong>for</strong> the three monochromatic waves studied and in all modes <strong>of</strong> motion. For the semisubmersible<br />

plat<strong>for</strong>m, the second order component <strong>of</strong> the unrestrained motions is higher than the first-order<br />

component <strong>for</strong> the less steep wave (period equal to 5s) in all modes except heave. For the steeper waves the<br />

importance <strong>of</strong> this component decreases with respect to the first order and is small <strong>for</strong> the steepest wave (<strong>of</strong><br />

period equal to 9s).<br />

The comparisons between first and second order quantities were also per<strong>for</strong>med <strong>for</strong> three Pierson-Moskowitz<br />

spectra with sixteen components. For the OC3-Hywind the second-order components are important in surge<br />

and pitch modes. In heave these components are smaller <strong>for</strong> the spectra with lower significant wave height and<br />

<strong>of</strong> the same importance as first order <strong>for</strong> the spectra with higher significant wave height (Hs=5m). The second<br />

order component <strong>of</strong> the excitation <strong>for</strong>ces and moments <strong>for</strong> the semi-submersible plat<strong>for</strong>m is higher than the<br />

first-order component <strong>for</strong> the spectra with lower significant wave heights (0.5m and 2.5m) <strong>for</strong> all modes except<br />

heave. For the spectra with Hs=5.0m, the second-order effects are <strong>of</strong> the same importance as the first-order <strong>for</strong><br />

surge, roll, pitch and yaw and dominant sway. In heave mode the effect <strong>of</strong> the second order component <strong>of</strong> the<br />

excitation <strong>for</strong>ce is very small in relation to the first-order.<br />

The unrestrained motions associated with the three spectra <strong>for</strong> both structures are very small. For the OC3-<br />

Hywind the second-order unrestrained motions are important <strong>for</strong> surge and pitch <strong>for</strong> the spectra with the lower<br />

significant wave heights (0.5m and 2.5m) and in heave <strong>for</strong> the spectra with significant wave height equal to<br />

5.0m. For the semi-submersible plat<strong>for</strong>m slow drift motions are identified with the second order component being<br />

dominant or <strong>of</strong> the same order <strong>for</strong> most <strong>of</strong> the modes <strong>for</strong> the three spectra.<br />

8.2.2 Nonlinear potential flow <strong>methods</strong><br />

The above study does not access any results associated with fully nonlinear potential flow hydrodynamic models.<br />

Ongoing research is being per<strong>for</strong>med at the University <strong>of</strong> Hamburg into a nonlinear seakeeping simulation<br />

technique by using a Rankine-Airy panel method [115]. The base flows from which the flow around the moving<br />

body is superimposed are not only source (and possibly vortex) flows, but also Airy waves. Nonlinear boundary<br />

conditions at the free surface (constant pressure, no flux through the surface) are satisfied numerically in each<br />

time step by superimposing Airy waves <strong>of</strong> different wave numbers and propagation directions. The amplitudes<br />

and phase angles <strong>of</strong> the Airy waves are not constant over time, but have to be computed from evolution equations.<br />

These are derived from the kinematic and dynamic free-surface conditions. The method is suitable <strong>for</strong><br />

arbitrary geometries and can deal with most <strong>of</strong> the be<strong>for</strong>e mentioned nonlinear effects in steep waves. This<br />

method can be effectively applied <strong>for</strong> the estimation <strong>of</strong> extreme behaviour <strong>of</strong> floating <strong>of</strong>fshore wind turbines in<br />

survival conditions.<br />

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