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The impact of removing the high-frequency spectral tail on rogue wave statistics

Published online by Cambridge University Press:  02 December 2022

Tianning Tang*
Affiliation:
Department of Engineering Science, University of Oxford, Oxford OX1 3PJ, UK
Dylan Barratt
Affiliation:
Department of Engineering Science, University of Oxford, Oxford OX1 3PJ, UK
Harry B. Bingham
Affiliation:
Department of Civil & Mechanical Engineering, Technical University of Denmark, Lyngby, DK 2800, Denmark
Ton S. van den Bremer
Affiliation:
Department of Engineering Science, University of Oxford, Oxford OX1 3PJ, UK Faculty of Civil Engineering and Geosciences, Delft University of Technology, 2628 CD Delft, The Netherlands
Thomas A.A. Adcock
Affiliation:
Department of Engineering Science, University of Oxford, Oxford OX1 3PJ, UK
*
Email address for correspondence: tianning.tang@eng.ox.ac.uk

Abstract

When making directional surface gravity waves in a wave tank or when initialising numerical simulations of the ocean, the wave spectrum is often curtailed suppressing higher frequencies and wavenumbers. We consider the impact of doing this by numerically simulating two seminal experiments, those of Onorato et al. (J. Fluid Mech., vol. 627, 2009, pp. 235–257, R2) and Latheef & Swan (Proc. R. Soc. A, vol. 469, no. 2152, 2013, p. 20120696). We simulate waves using a fully nonlinear potential-flow model. We find that curtailing the spectrum can have a significant impact on the subsequent evolution. In particular, for cases where the spectrum has been curtailed, the nonlinear physics produces significantly more extreme or rogue waves than are observed in the case where the full spectral tail was included in the initial conditions, and this difference persists over tens of periods after the waves are initialised. This suggests that sea states that are ‘out of equilibrium’ (i.e. with their tails removed) can produce a greater number of rogue waves. We show this can also have an impact on predicted loads on offshore infrastructure.

Information

Type
JFM Papers
Creative Commons
Creative Common License - CCCreative Common License - BY
This is an Open Access article, distributed under the terms of the Creative Commons Attribution licence (http://creativecommons.org/licenses/by/4.0), which permits unrestricted re-use, distribution and reproduction, provided the original article is properly cited.
Copyright
© The Author(s), 2022. Published by Cambridge University Press.
Figure 0

Table 1. Dimensions of the laboratory experiments (exp.) and the numerical (num.) domains. Here ST and LT denote short-tail and long-tail cases, respectively.

Figure 1

Table 2. Initial sea-state parameters used in this study, where $\omega _{0}$ is the peak frequency, $k_0$ the peak wavenumber based on the linear dispersion relationship. Water depth, $d$, is presented non-dimensionally. Spreading shows the equivalent spreading angles based on the spreading functions (2.2). The percentage of total energy below the cutoff frequency is given in the rightmost column.

Figure 2

Figure 1. Initial omni-directional frequency variance density spectra for the simulations of the experiments of (a) LS13 and (b) O09.

Figure 3

Figure 2. For O09, crest exceedance probabilities at four different distances from the paddle (locations of gauges in the experiments of O09): (a) $x=3.1\lambda _0$, (b) $x=6.3\lambda _0$, (c) $x=12.6\lambda _0$, (d) $x=22.3\lambda _0$ for ST and LT simulations. The shaded regions correspond to 90 % confidence intervals for the simulations based on the bootstrap method. The results O09$_{\rm ST}$ and O09$_{\rm LT}$ are obtained through fully nonlinear potential-flow simulations. Also shown are the experimental results from O09.

Figure 4

Figure 3. For O09, wave crest amplitude at the $10^{-3}$ crest exceedance probability level for ST and LT simulations. The shaded regions correspond to 90 % confidence intervals for the simulations based on the bootstrap method. Also shown are the experimental results from O09. A zero-phase shift Fourier filter is applied to smooth out short-term fluctuations within the length scale of $0.4\lambda _0$.

Figure 5

Figure 4. For LS13, crest exceedance probabilities at four different distances from the paddle: (a) $x=0.3\lambda _0$, (b) $x=1.075\lambda _0$ (location of the gauge in the experiments of LS13), (c) $x=1.76\lambda _0$, (d) $x=16.1\lambda _0$. The shaded regions correspond to 90 % confidence intervals for the simulations based on the bootstrap method. The results LS13$_{\rm ST}$ and LS13$_{\rm LT}$ are obtained through fully nonlinear potential-flow simulations. Also shown are the experimental results from LS13.

Figure 6

Figure 5. For LS13, wave crest amplitude at the $10^{-3}$ crest exceedance probability level for ST and LT simulations. The shaded regions correspond to 90 % confidence intervals for the simulations based on the bootstrap method. Also shown are the experimental measurements from LS13. A zero-phase shift Fourier filter is applied to smooth out short-term fluctuations within the length scale of $0.4\lambda _0$.

Figure 7

Table 3. Wavenumber cutoffs used in the literature to simulate O09.

Figure 8

Figure 6. Kurtosis evolution for $\text {O09}_{\text {ST}}$ (red line) and $\text {O09}_{\text {LT}}$ (blue line) compared against other studies. (a) The cases with truncated tails; these cases are Xiao et al. MNLS ($-\!-\!-$), Toffoli et al. MNLS ($\circ$) and Barratt et al. MNLS ST case (red $-\!-\!-$). (b) The cases without truncated tails; these cases are Xiao et al. HOS (——), Toffoli et al. HOS ($\times$) and Barratt et al. MNLS LT case (blue $-\!-\!-$). The shaded bands represent 95 % confidence intervals based on the standard deviation of different realisations. The coloured dash line indicates the peak kurtosis value for $\text {O09}_{\text {ST}}$ and $\text {O09}_{\text {LT}}$, respectively.

Figure 9

Figure 7. Excess kurtosis evolution for case $\text {O09}_{\text {ST}}$ (red line) and case $\text {O09}_{\text {LT}}$ (blue line) compared against the solution of Fedele (2015) based on the initial wave spectrum at $x=0\lambda _0$ for both cases. The shaded bands represent 95 % confidence intervals based on the standard deviation of different realisations.

Figure 10

Figure 8. Evolution of kurtosis for case $\text {LS13}_{\text {ST}}$ and case $\text {LS13}_{\text {ST}}$ compared with the predictions of Fedele (2015) based on the initial wave spectrum at $x=0$ for both cases. The shaded bands represent 95 % confidence intervals based on the standard deviation of different realisations.

Figure 11

Figure 9. (a) Spatial evolution of significant steepness $\xi$ for $\text {O09}_{\text {ST}}$, $\text {O09}_{\text {LT}}$ and experimental results presented in O09. The results are normalised by the initial value of $\text {O09}_{\text {LT}}$. (b) Spatial evolution of spectral bandwidth parameter $\nu$ for $\text {O09}_{\text {ST}}$, $\text {O09}_{\text {LT}}$ and experimental results presented in O09. The results are normalised by the initial value of $\text {O09}_{\text {LT}}$.

Figure 12

Figure 10. (a) Spatial evolution of significant steepness $\xi$ for both $\text {LS13}_{\text {ST}}$ and $\text {LS13}_{\text {LT}}$ cases normalised by the initial value of $\text {LS13}_{\text {LT}}$. (b) Spatial evolution of spectral bandwidth parameter $\nu$ for both $\text {LS13}_{\text {ST}}$ and $\text {LS13}_{\text {LT}}$ cases normalised by the initial value of $\text {LS13}_{\text {LT}}$.

Figure 13

Figure 11. For O09, the overturning moment magnitude exceeded 0.5 % of the total simulation time normalised by its initial value (at $x=0$) for $\text {O09}_{\text {LT}}$. The shaded bands represent 90 % confidence intervals based on the bootstrap method.

Figure 14

Figure 12. For LS13, the overturning moment magnitude exceeded 0.5 % of the total simulation time normalised by its initial value (at $x=0$) for $\text {LS13}_{\text {LT}}$. The shaded bands represent 90 % confidence intervals.