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Iso-surfaces α = 0.5 -light blue, ω = 3000 s −1 -orange, t = 0.34 s, implicit LES.

Iso-surfaces α = 0.5 -light blue, ω = 3000 s −1 -orange, t = 0.34 s, implicit LES.

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Conference Paper
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The work presented here forms part of a project focusing on the development of cost-effective measures of classifying the noise levels from ship propellers with the use of numerical techniques available in OpenFOAM software. It is also related to the on-going research within the Faculty of Engineering and the Environment at the University of Southa...

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... interesting observation may be made when comparing the cavity extents just after the point of maximum lift for both implicit and explicit LES simulations, shown in Fig- ures 4 and 5, respectively. At this stage the attached sheet has been cut by the re-entrant jet close to the leading edge of the foil and starts being convected downstream to form a cloud. ...

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Citations

... Cavitation is a common physical phenomenon that occurs when the local fluid pressure drops to the saturated vapour pressure (Arndt, 2002;Long et al., 2017Long et al., , 2018. In engineering applications, cavitating flows are typically associated with complex shedding behavior (Correction Ji et al., 2014;Chen et al., 2021a;Ji et al., 2010), violent pressure fluctuations Wang et al., 2017), and high turbulence Coutier-Delgosha et al., 2003;Lidtke et al., 2014). The resulting transient pulsating force (Yu et al., 2019;Li et al., 2020a) can cause severe damage and noise pollution to hydraulic working parts, such as propellers (Sezen et al., 2021), pumps (Liu and Tan, 2020a), water turbines Tan, 2018, 2020b), and ship appendages (Ianniello et al., 2014a), among others. ...
... The time-averaged lift coefficient predicted by the PANS calculations was about 12% lower than the experimental value. Lidtke et al. (2014) investigated the same cases using three different turbulence models and observed clear differences in the predictions of the all approaches. It was mentioned that judging from the substantial difference between the RANS and LES approaches in both the lift and cavity volume variations, one may conclude that the latter should be used for this purpose whenever possible. ...
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... • parts of this work have been published as: [119], [120], [121], [122] [124], [125], [126], [133] Signed:.. ...
Thesis
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Anthropogenic noise from a variety of merchant ships has been reported to be a major factor adversely aecting marine organisms. Consequently, scientists and regulators have become more vocal about encouraging, and possibly enforcing, quieter ships in the future. For this to be feasible from an engineering standpoint, a range of numerical methods must be made available to allow acoustic performance of vessels to be evaluated at the design stage. Cavitation is a major contributor to the hydroacoustic signature of a merchant vessel. The reason for this is the relatively high drop of pressure induced by the propeller, which in turn promotes the growth of vapour bubbles and cavities, oscillation and collapse of which act as strong acoustic sources. The entire process is made more dynamic by the non-uniform wake of the ship, propeller rotation, as well as the fact that vessels travel in a seaway. Because of its complexity, the problem of marine propeller noise is thus not widely studied numerically, which translates to the lack of tools readily available to designers willing to reduce the noise generated by ships. A set of numerical utilities are proposed which could be employed at the late design stage of a merchant ship in order to allow the designer to estimate the radiated noise and make informed decisions on how to improve the design. The methodology involves solving the turbulent flow over the propeller using Detached Eddy Simulation (DES) and modelling cavitation using a mass-transfer model. The porous Ffowcs Williams-Hawkings acoustic analogy is used to infer far-eld radiated noise caused by the blade rotation, pulsating cavitation, as well as non-linear noise sources in the propeller slip-stream. The cavitation model is also extended to incorporate Lagrangian bubbles dispersed downstream of the large cavities modelled using the baseline Schnerr-Sauer model via the volume fraction equation approach. This allows the broadband nature of cavitation noise to be captured. The methods are applied to a NACA 66 and the Delft Twist 11 hydrofoil test cases. Although there are limited validation data allowing all of the methods to be validated simultaneously, relatively good agreement is seen at intermediate validation stages. These include comparing the non-cavitating noise of the Insean E779a propeller to reference data, conducting acoustic predictions for idealised acoustic sources, as well as comparing cavitation patterns, cavity cloud shedding frequencies, and induced pressures to experimental data for hydrofoils and propellers. It is concluded that the presented methodology may be used to predict low-frequency noise due to cavitation in a relatively robust manner, although the method is yet to be tested and validated on more complex geometries. The hybrid Eulerian-Lagrangian model is still at an early stage and a range of areas for improvement have been identified, such as implementation of more realistic cavity break-up models as well as better coupling between the fluid and bubble solvers. Nonetheless, the method is demonstrated to be a promising tool at tackling the broadband cavitation noise components as it can capture the contribution of the mass of small, oscillating bubbles on the radiated pressure which would otherwise be unaccounted for in the baseline Eulerian framework.
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... This indicates that the presented method is well suited to provide information useful throughout the propeller design cycle. Unfortunately, unsteady RANS has been recognized as not being able to predict the unsteady behaviour of the cavities particularly well (Bensow, & Liefvendahl2008) (Lidtke et al. 2014), nor is it capable of resolving the tip vortex regions accurately. Both of these phenomena may be expected to play a significant role in the noise generation mechanisms of a marine propeller (Salvatore 2009). ...
... This indicates that the presented method is well suited to provide information useful throughout the propeller design cycle. Unsteady RANS is not able to predict the unsteady behaviour of the cavities particularly well (Bensow and Liefvendahl, 2008;Lidtke et al., 2014), nor is it capable of resolving the tip vortex regions accurately. Both of these phenomena may be expected to play a significant role in the noise generation mechanisms of a complete marine propeller (Salvatore, 2009). ...
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Two computational studies are presented in this paper. First, the Potsdam Propeller Test Case which is used to demonstrate the capabilities of mass transfer cavitation models, more precisely the model by Sauer and Schnerr, in tackling the problem of marine propeller cavitation. It is shown that the extents of the predicted cavitation regions agree well with the experiment but suffer from the fact that the tip vortices and the associated low pressure regions are under resolved when URANS is utilised. Next, preliminary results from the study of cavitation noise modelling attempt are presented for a NACA 0009 section, used as a simplified representation of a propeller blade. Large Eddy Simulation and Ffowcs Williams-Hawkings porous acoustic analogy are used in order to estimate the cavitation-induced noise. Results indicate that the discussed approach provides the means for identifying low-frequency noise generation mechanisms in the flow, yielding sound pressure levels of the order of 40 dB re 20 microPa, but does not allow for finescale bubble dynamics to be resolved. One may conclude that the discussed approach is a viable option to predict large parts of marine propeller noise spectra but further work is needed in order to account for the high frequency components.
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