# Validation Tests for Potential Flow Models with Morison Drag (LPMD)

The linear potential flow model in QBlade (QB) (see Linear Potential Flow Theory) was validated in a series of test load cases using two different turbine models: a spar buoy and a semisubmersible. The linear potential flow model was enhanced with quadratic drag forces via the Morison equation (see Morison Equation) and is termed LPMD in this document. The load cases were chosen with increasing complexity to make sure the individual modules were working correctly.

The results were validated against the open-source aero-hydro-elastic code OpenFAST (OF) 1 (version 2.5.0). The same turbine models and test cases were setup and used in QB and OF. Not all of the hydroelastic modelling capabilities of QB are present in OF. When validating certain hydrodynamic models, the hydrodynamic capabilities of QB were adapted to reflect those of OF to have a better comparison. These modifications are mentioned in the appropriate load cases below.

In the following sections, the results for each model are presented.

## OC3 Spar Buoy LPMD Model

The first model, named OC3 model in this document, is the floating 5 MW wind turbine mounted on a spar buoy from the OC3 Report 2. This model was considered so that we have a simple geometry to test the different hydrodynamic models. Fig. 156 shows the OC3 LMPD model within the QB GUI. The substructure was considered rigid in this model to evaluate only the hydrodynamic modules. For this model, the mooring system was modeled explicitly and the localized buoyancy model was used.

### OC3 LPMD No Wave Tests

The no wave tests are split into two parts, the first and main part consists in free decay tests in still water. The second part considers the turbine reaction to no wave and constant current conditions. We will describe first the results from the decay tests and later present the results for the constant current tests.

#### OC3 LPMD Free Decay Tests

The free decay tests simulate the turbine model in free decay from an initial position in still water condition. No aerodynamic loads were considered in the decay tests. All the 6 degrees of freedom (DOFs) are considered for in the decay tests. The evaluation of the results is done 1) visually, by inspecting the time series of all isochronic DOFs and 2) quantitatively, by analyzing the eigenfrequency and damping of the disturbed DOF. The latter analysis was done according to the procedure presented in 3.

Fig. 157 to Fig. 159 show the time series for the decay tests of the surge, heave and pitch DOFs. From these figures we can see that the predictions from QB and OF are practically identical. This is not only the case for the initially disturbed DOF but for the other DOFs as well. In the surge and pitch decay tests, there is a small offset between the heave time series. This offset comes from the different way the buoyancy is calculated between OF and QB. In OF, the buoyancy is accounted for by linearized stiffness matrices. In QB, the buoyancy forces is taken are calculated explicitly by taking into account the locally displaced water volume.

The decay tests for the other three DOFs (sway, roll, yaw) were also simulated. The time series are not included in this document since the findings are very similar.

Fig. 160 to Fig. 162 show the corresponding tensions at the fairlead and anchor locations of the mooring systems for the surge, heave and pitch decay tests. We can see good agreement between both codes. Again, for the heave decay tests, there is a small offset in the tensions between the QB and OF simulations. It can be explained by the small offset in the heave neutral position between both codes and the different approaches used in both codes to model the mooring system.

The decay tests were also analyzed quantitatively by comparing the eigenfrequencies and damping characteristics of the floater for the initially displaced DOFs. Fig. 163 shows the results for the six performed decay tests. We can see in this figure that the normalized eigenfrequencies agree very well between both codes. There are significant differences in the damping characteristics, especially for the surge, sway, heave and yaw DOF.

The differences are assumed to come from the different mooring system models. OF uses MoorDyn, which uses a lumped-mass formulation for modelling axial elasticity 4. QB uses a cable structural formulation (see Multi Body Beam Formulation) coupled with the Morison equation (see Morison Equation) to account for the hydrodynamic forces on the mooring system. In order to test if the mooring system formulation causes the different damping behavior, we replaced the mooring system models with linear stiffness matrices in both codes. Since there is a significant linear damping term in the hydrodynamic matrices in the surge, sway, heave and yaw DOFs, a linear damping relation was assumed for the evaluation of the time series.

Fig. 164 shows the normalized eigenfrequencies and linear damping characteristics for the models with linearized mooring systems. We can see now that the values for all DOFs except the yaw DOF align. For this turbine model the yaw DOF does not couple with the other DOFs and is almost exclusively determined by the stiffness, damping and inertia matrices, since the quadratic damping term of the Morison equation is not applied to cylinder rotations. So the decay behavior can be calculated analytically. Using the stiffness, inertia and damping values and adding the rotational inertia of the turbine, an analytic eigenfrequency of 0.118 Hz was determined. This value is only 3% off from the values gotten in the QB and OF calculations. The analytical damping ratio is 4.4%. This value differs from the one obtained in QB simulations by 0.5% and from the one by OF simulations by 17%. It is therefore assumed that the value obtained by QB simulations is the correct one.

#### OC3 LPMD Current-Only Tests

The second part of the no wave tests comprised constant current tests. For these tests, two current profiles were selected according to 5: a power-law profile – representing a tidal current velocity – and a linear profile – representing a wind-generated current (see Currents). The current direction is aligned with the positive surge direction. The turbine was initially in its original undisplaced position and the simulations included the transient response to the current profiles. No aerodynamic loads were applied in this case.

Fig. 165 shows the time series of the wind-generated current test with a surface current magnitude of 3 m/s and decrease rate of 0.2 1/s. We can observe in this figure that the turbine behaves almost identically for the affected DOFs (surge and pitch) when simulated with QB and OF. The different behavior in the heave DOF can be attributed to the different ways the buoyancy is modelled in QB and OF. The right column plots of Figure 25 show the water particle velocities at three different locations along the turbine substructure: at 0 m, at -10 m and at -20 m. We can see that the water velocities do not fully match. The reason for this is twofold. Firstly, the water particle velocities from QB are shown in the moving coordinate system of the substructure while in OF a fixed set of positions is used for the water particle velocity output. Secondly, OF interpolates the water particle velocities to the output nodes while QB shows the velocities for the center of the member that is closest to the selected output location. In the case of Fig. 165, the center member location and the velocity output location was slightly different.

### OC3 LPMD Regular Wave Cases

The regular wave cases aim to validate the implementation of the first-order wave excitation forces in QB. This done in load cases where a single wave train with varying amplitude, period and direction is used to model the sea state. In order single out the effect of the excitation force implementation, the respective models in both simulation tools are set up to be as similar as possible. Therefore, the mooring system and the buoyancy are modeled with a linearized stiffness matrix. Both tools make use of the same excitation force impulse response function (IRF) computed in WAMIT 6. No wave stretching model was used in QB so that the modelling considerations between QB and OF were as close as possible (see Kinematic Stretching). OF does currently not allow wave stretching models to be implemented in HydroDyn 7. Similar to the free decay tests, no aerodynamic loads were considered. The validation is done by analyzing the time series and frequency spectra of the excited OC3 model.

Fig. 166 and Fig. 167 show the time series and corresponding spectra of the three DOFs (surge, heave, pitch) excited by an incoming wave from 0° direction for two regular wave cases. The first case has a wave height of 6 m and a period of 10 s and the second case has a wave height of 8 m and a period of 12 s. In both cases, an initial transient is present and completely dies out after approximately 300s. This explains the additional peaks at lower frequencies than the wave frequency in the respective spectral plots. Afterwards, a constant frequency excitation by the linear wave is present in all DOFs. It can be noted that the translations and rotations of the floater are predicted in an identical manner between both tools. Hence, a correct implementation of the first-order wave excitation loads may be concluded. It can be further noted that changing the wave height and period does not induce any differences between both tools.

The next feature requiring validation is the influence of waves that approach the floater with an oblique angle. The excitation input file provides IRFs with a degree spacing of 10 degrees (-180°:10°:180°). Thus, a wave that heads in from an intermediate angle requires interpolation of the IRF. In order to validate this, Fig. 168 shows the time series of all DOFs for a regular wave with a wave height of 6 m, a period of 10 s and a wave angle of 45 degrees. Once again both tools show very good agreement in the floater response. Very slight differences in the yaw DOF might be attributed to differences in the interpolation algorithms.

### OC3 LPMD Irregular Wave Cases

The validation of the first-order excitation loads in irregular waves was performed in a similar fashion to the regular wave cases. Accordingly, the mooring system and buoyancy are modelled via linearized matrices. The IRFs were precomputed in WAMIT and are identical to the ones used in OF. At this point it is worth mentioning that the algorithmic approach doesn’t change within the hydrodynamic model of QB for an irregular wave field compared to a wave field consisting of a single wave train. The reason is, that the excitation loads are computed for every single wave train and superposed linearly (see Linear Wave Theory). Two separated cases are analyzed. Firstly, an irregular wave field based on a JONSWAP spectrum with uni-directional waves is considered. Secondly, a directional spread of the wave trains is added in order to further validate the direction-dependent calculation of the wave loads. To increase the statistical validity of the results, six runs were carried out for each simulated case. The significant wave height amounts to \(H_s\) = 6 m and the peak spectral period to \(T_p\) = 10 s. A peak enhancement factor of \(\gamma\) = 3.3 was chosen. The floater response in all 6 DOFs will serve as the validation parameter. Finally, statistical parameters of the floater response and the tower base loads will be presented.

Fig. 169 shows the averaged wave fields that serve as an input to the calculation of the wave forces. In Fig. 170 the floater response for an irregular wave field with uni-directional waves is presented. The three excited DOFs (surge, heave, pitch) show good accordance between QB and OF. The results are averaged over the last 250 s of the aforementioned six runs, each with 800 s total duration. The peak at the floater eigenfrequency arises due to not completely damped out initial transients.

Fig. 171 shows the PSDs of the floater response for multi-directional waves in all 6 DOF s. To reduce the influence of the initial transient, the total simulation length was set to 1200s. Again. The PSDs are averaged over the last 300s of six different simulations.

Fig. 172 shows the time average, the standard deviation as well as minima and maxima of the floater response in the 6 DOFs of both tools. Small deviations between the codes are visible but in general a similar behavior is visible once again. An exact matching between these statistical parameters may not be expected as they depend on the occurrence of severe wave groups. A longer simulation time would presumably increase the agreement between the compared codes.

#### OC3 LPMD Irregular Waves with Current

For the irregular wave test cases, a combination of wave and currents was also considered. For this case, a JONSWAP spectrum with a significant wave height of \(H_s\) = 6 m, a peak spectral period of \(T_p\) = 10 s and a value of \(\gamma\) = 3.3 was again chosen. This wave spectrum was combined with a constant tide-induced current with a power law of 1/7th and a surface current value of 0.5 m/s. The wave and current directions aligned with the positive surge direction. Six repetitions were considered to account for the statistical variance of irregular waves. In this test case, the same wave elevation input was used for OF and QB simulations. Again, no aerodynamic loads were applied on the turbine. The mooring systems were modelled explicitly.

We can see in Fig. 173 the averaged PSDs of the six repetitions for all DOFs for both simulations. The figure shows that the substructure dynamics for the relevant DOFs under irregular sea states and constant currents is virtually identical if simulated with OF or QB.

Fig. 174 shows the averaged PSD of the corresponding tensions at the fairlead and anchor positions for the irregular wave plus current cases. We can see in this figure that there is a larger variation of the fairlead and anchor tensions for the downwind mooring lines (lines 2 and 3). This difference can be attributed to the different mooring system modelling that is present in QB and OF.

## OC4 Semisubmersible LPMD Model

The second model considered in this validation – named OC4 model in this document – is the floating 5 MW wind turbine mounted on a semisubmersible substructure from the OC4 Report 8. The geometry of the OC4 model within the QB GUI is shown in Fig. 175. This figure shows clearly the more complicated geometry of the turbine model. Hence, the hydrodynamic behavior of this model is expected to be more complicated. The substructure was again considered rigid in this model to evaluate only the hydrodynamic modules in this more challenging geometry. Unless otherwise stated, the mooring system was modeled explicitly and the localized buoyancy model was used for this model.

### OC4 LPMD Free Decay Tests

For this model, decay tests were again performed in still water for four DOFs and compared to the same simulations performed with OF. Again, the main difference between both codes in these tests were the mooring system modelling and the way the buoyancy was calculated.

Fig. 176 to Fig. 178 show the free decay tests for the surge, pitch and yaw DOF. We can see again that the results for QB and OF are very similar. Especially for the disturbed DOFs and the DOF that are directly coupled to them, the differences between both codes are small. We note again a small difference in the mean of the heave position. This comes from the different buoyancy models used in QB and OF.

Fig. 179 shows the corresponding tensions at the fairlead and anchor locations of the mooring systems for the surge decay tests. Again, we can see good agreement between both codes. There is an offset in the tensions between the OF and QB simulations. This can be explained by the small offset in the heave neutral position between both codes and also from the different modelling approaches used for the mooring system. The tensions for the other DOFs were also analyzed but not included here for brevity reasons. The findings of these other decay tests are equivalent to the ones shown in Fig. 179.

The numerical values for the frequencies and damping coefficients of the decay tests were also analyzed for these cases. The results are shown in Fig. 180. In this figure, we can see that the relative values of eigenfrequencies between both codes are close to 1. This agreement can also be seen visually in the figures above. The same can be said for the quadratic damping term. As for the linear damping term, we can see that there are some differences between the relative values of both codes. As with the OC3 model, the differences can be traced back to the different mooring system modeling used in both codes.

### OC4 LPMD Regular Wave Tests

The regular wave tests were performed with linear Airy waves for two selected cases. One case had a wave height of \(H\) = 6 m and a period of \(T\) = 10 s. The second case had a wave height of \(H\) = 8 m and a period of \(T\) = 12 s. For these cases, a simulation time of 1000 s was chosen and the first 300 s were discarded. This is because we were only interested in the response of the turbine once the initial transients were settled. No aerodynamic loads were considered and the wave direction was chose to coincide with the direction of the positive surge DOF. As for the wave tests for the OC3 model, no wave stretching model was applied in QB so that the modelling considerations between QB and OF were as close as possible.

It should be noted here that for the more complex geometry of the OC4 model, the buoyancy model will affect the response of the substructure to the incoming waves. This comes from the fact that the bodies that provide buoyancy for the OC4 model are spatially distributed. As the wave passes the substructure, the local buoyancy forces induce additional forces and moments that affect the principal DOFs of the substructure. These forces and moments are not accounted for if only a linear constant force and restoring force matrix is used to account for the buoyancy.

To verify the hydrodynamic models for the radiation forces, the wave excitation forces and the diffraction forces as well as the quadratic drag forces from the Morison equation, a modified OC4 LPMD model was built that includes a linear buoyancy model in a similar fashion as OF. This model was termed “QB Lin” in this section. Additionally, the complete OC4 LPMD model with the distributed buoyancy forces was also modelled. This model was used to analyze the effect of the buoyancy model on the substructure response and on the tensions of the mooring system.

Fig. 181 shows the response of the surge, heave and pitch DOF as well as the wave elevation for the test case with \(H\) = 6 m and \(T\) = 10 s. We can see in this figure that the response of the linear buoyancy model in QB (QB Lin) is practically identical to the response in OF. This validates the hydrodynamic modules for radiation, diffraction and wave excitation forces as well as the quadratic drag forces in the more complicated geometry of the OC4.

If we use the local buoyancy model in QB (QB Loc), we can see in Fig. 181 that all the relevant DOFs are affected. We can see that the surge DOF oscillates with a larger amplitude and reaches more negative values compared to the linear buoyancy model. In addition, the amplitude and phase of the pitch and heave DOFs change if we use the local buoyancy model. In particular, the amplitude of both DOFs is smaller and the phase shifts with a positive magnitude. This behavior was not seen in the regular wave calculations of the OC3 model because all the buoyancy forces were concentrated on the spar axis and were not spatially distributed.

This different behavior due to the local buoyancy model also has an effect on the tensions of the mooring system. In Fig. 182 we can see the mooring line tensions of the regular sea state shown in Fig. 181. We can see that there is the slightly higher average value of the mooring tension in the OF calculations compared to the QB Lin calculations. This offset was also identified in the decay tests and is attributed to the different mooring system modelling in both codes. Important here is that the phase and magnitude of the tensions is comparable in with the linear buoyancy model.

This behavior changes if we include the local buoyancy model. Here, the amplitude of the tension from mooring line 2 increases significantly compared to the QB Lin simulations. For the mooring lines 1 and 3, the effective amplitude of the tension oscillations gets reduced due to an additional oscillation that is shifted in phase. These differences can be attributed to the different response pattern in heave and pitch of the OC4 model when the local buoyancy is used.

Fig. 183 and Fig. 184 show the relevant DOFs and mooring line tensions for the regular sea state with \(H\) = 8 m and \(T\) = 12 s. We can again see that the response of QB Lin is comparable to OF in both the substructure dynamics and the tensions of the mooring lines.

The response of the substructure if the local buoyancy model is used changes even more drastic for this test case. In Fig. 183 we see that the mean surge displacement of the QB Loc simulations is now negative compared to the positive mean surge displacement of the QB Lin simulations. Now, the heave and pitch DOF have a larger amplitude compared to the QB Lin simulations and there is again a positive phase shift.

The effects on the mooring line tensions can be seen in Fig. 184. In this figure, it can be clearly seen that the tension of the mooring line 2 is significantly affected for this test case. The amplitude of the oscillation is more than doubled in the QB Loc simulations compared to the QB Lin simulations.

### OC4 LPMD Irregular Wave Tests

The OC4 LPMD model was also validated for irregular wave sea states. Six random sea states with a JONSWAP spectrum with \(H_s\) = 6 m, \(T_p\) = 10 s and \(\gamma\) = 3.3 were used. The simulation length was 1200 s and the first 400 s were not considered in the analysis to discard initial transient effects. Again, no aerodynamic loads were considered in these cases and the wave propagation direction was chosen to be aligned with the positive surge direction. Additionally, no wave stretching model and no second order wave forces were included in the simulations. The response of the turbine model was done in a statistical manner by comparing the averaged PSDs of the DOFs.

As we could see in the regular wave validation tests, the buoyancy model has an important effect on the substructure response and the mooring line tensions. For these calculations, the linear buoyancy model was used in QB. Although the local buoyancy calculation is deemed more accurate, we chose the linear model to allow for a better comparison between OF and QB. In addition, the mooring system was also simulated using linear matrices in both codes. We chose to do this to again align the modeling approaches as much as possible. The mooring system is considered validated based on the validation tests done beforehand.

Fig. 185 shows the averaged PSDs of all six DOFs for the irregular sea states. In this figure, the results from three different simulation setups are shown. The original OC4 LPMD model in QB and OF is labeled accordingly in this figure. Additionally, the results QB MSL are also presented in this figure. In the latter simulation setup, the quadratic forces of the Morison equation are calculated considering that the Morison element are wetted up to the mean sea level. This effectively neglects the local wave elevation when calculating the wetted surface of the substructure that will be considered for the Morison drag calculations. This approach is the one implemented in OF. In contrast, QB considers the local wave elevation (incl. wave stretching) to determine the wetted surface of the elements and apply the Morison forces. See modelin considerations in Morison Equation for more details. The setup QB MSL was thus chosen to have a simulation setup that matches the OF modelling.

We can see in Fig. 185 that the averaged PSD of all DOFs are very similar between the OF and QB simulations. There is a distinct difference at the low frequency regime of the surge DOF. The peak corresponding to the surge eigenfrequency is significantly larger in the QB simulations compared to the OF simulations. Notably, if we change the QB simulations to consider the wetted surface up to the mean sea level (QB MSL), the difference in the peak at the surge eigenfrequency vanishes.

This phenomenon can be explained as follows. By considering the Morison drag calculations up to the local wave elevation only, there will be a net positive drag force in the surge direction. This is because as the wave particles retract during the trough of the wave, less surface will be wetted and less drag force will act on the substructure compared to the case where the substructure sees a wave crest. In the latter case, the wetted surface will encompass up to the mean sea level (no wave stretching). The irregular sea state will include time periods where the wave heights are large and time periods where the wave heights are small. The former scenario leads to high average mean surge forces while the latter scenario to low mean surge forces. The restoring forces from the linear mooring system will therefore let the OC4 model oscillate at its surge eigenfrequency when the average surge force is temporarily small. This non-linear phenomenon cannot happen it the wetted surface is considered constant at all times.

### OC4 LPMD Second-Order Wave Excitation Forces

Second-order hydrodynamic loads play an increasing role for semi-submersible offshore structures such as the OC4 model. Duarte et al. 9 even state that the floater response is dominated or at least in impacted in the same order of magnitude by the second order hydrodynamic loads as by their first order relatives. Bearing this in mind, a first evaluation of the implementation of the second-order wave load module, described in Linear Potential Flow Theory seems reasonable on the OC4 platform. In the following, the force spectra of the second order wave loads acting in all 6 DOFs on the OC4 model in irregular waves are presented. The previously used JONSWAP spectrum with \(H_s\) = 6 m, \(T_p\) = 10 s and \(\gamma\) = 3.3 once again was used to create the uni-directional (from 0 deg) wave field. The used QTFs were computed in WAMIT and are identical between QB and OF.

Fig. 186 shows the similarity in the results between QB and OF. Both tools agree very well in the excited frequencies and also in the respective amplitudes. We can further see, that the sum- and difference frequency loads clearly excite the floater outside of the present frequencies of the JONSWAP spectrum, especially in the pitch and heave DOF.

Fig. 187 shows the result of the approximated second-order difference-frequency loads in all 6 DOFs using Newman’s approximation. Again, strong similarities between the used simulation tools become evident. It also can be noted that the difference loads contain energy at frequencies lower than those present in the JONSWAP spectrum.

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