*Article* **Towards a Realistic Estimation of the Powering Performance of a Ship with a Gate Rudder System**

**Noriyuki Sasaki 1, S. Kuribayashi 2, M. Fukazawa <sup>3</sup> and Mehmet Atlar 1,\***


Received: 11 December 2019; Accepted: 12 January 2020; Published: 15 January 2020

**Abstract:** This paper presents an investigation on the scale effects associated with the powering performance of a Gate Rudder System (GRS) which was recently introduced as a novel energy-saving propulsion and maneuvring device. This new system was applied for the first time on a 2400 GT domestic container ship, and full-scale sea trials were conducted successfully in Japan, in 2017. The trials confirmed the superior powering and maneuvring performance of this novel system. However, a significant discrepancy was also noticed between the model test-based performance predictions and the full-scale measurements. The discrepancy was in the power-speed data and also in the maneuvring test data when these data were compared with the data of her sister container ship which was equipped with a conventional flap rudder. Twelve months after the delivery of the vessel with the gate rudder system, the voyage data revealed a surprisingly more significant difference in the powering performance based on the voyage data. The aim of this paper, therefore, is to take a further step towards an improved estimation of the powering performance of ships with a GRS with a specific emphasis on the scale effect issues associated with a GRS. More specifically, this study investigated the scale effects on the powering performance of a gate rudder system based on the analyses of the data from two tank tests and full-scale trials with the above-mentioned sister ships. The study focused on the corrections for the scale effects, which were believed to be associated with the drag and lift characteristics of the gate rudder blades due to the low Reynolds number experienced in model tests combined with the unique arrangement of this rudder and propulsion system. Based on the appropriate semi-empirical approaches that support model test and full-scale data, this study verified the scale effect phenomenon and presented the associated correction procedure. Also, this study presented an enhanced methodology for the powering performance prediction of a ship driven by a GRS implementing the proposed scale effect correction. The predicted powering performance of the subject container vessel with the GRS presented an excellent agreement with the full-scale trials data justifying the claimed scale effect and associated correction procedure, as well as the proposed enhanced methodology for the practical way of predicting the powering performance of a ship with the GRS.

**Keywords:** gate rudder system; flap rudder; energy saving device; ducted propeller; maneuvring device; powering performance; scale effects; laminar separation

#### **1. Introduction**

#### *1.1. Gate Rudder System*

A gate rudder system (GRS) is a rather novel but straightforward arrangement of the ship rudder and propeller to act as an attractive and sound energy-saving propulsion and maneuvring device (ESMD), for example, [1–3]. In this system, the classical single-rudder behind the propeller arrangement is replaced by twin-rudder blades with asymmetric cross-sections which are positioned on either side of the propeller. The two rudder blades encircle the propeller at the upper half of the propeller plane, as well as at both sides, such as a separated duct which is split into two sections with no bottom part. The arrangement of the gate rudder system (GRS) on the "Shigenobu" is shown in Figure 1a (left) in contrast to the conventional (flap-) rudder system (CRS) of the "Sakura" in Figure 1b (right). Shigenobu has the world's first GRS installed on it while her sister ship (Sakura) has a conventional rudder system (CRS) with the same hull and engine particulars. The principal dimensions of both vessels are presented in Table 1, Sasaki et al. (2019) [4].

**Figure 1.** (**a**) Gate rudder system (GRS) on coastal container ship "Shigenobu." and (**b**) conventional flap-rudder system (CRS) on sister container ship "Sakura.".


**Table 1.** Principal characteristics of Shigenobu and Sakura.

Each rudder blade of the GRS can be controlled individually to affect the direction of the propeller's slipstream (i.e., to vector), and hence to steer the vessel with increased maneuvring and motion control capability. The GRS, therefore, takes advantage of additional thrust generated by the two rudder blades, in contrast to the extra resistance that results from the conventional rudder. This is somewhat similar to the ducted propulsor but with a much larger propeller diameter as compared with the traditional ducted propeller with less surface area, and hence improves the efficiency significantly. The GRS, therefore, can be categorized as a new "open-type ducted propeller" which is distinct from a conventional "closed-type ducted propeller" (e.g., Kort Nozzle) and a "front-type ducted propeller" (e.g., the Becker Mewis Duct or SILD and Sumitomo Integrated Lammern Duct), as shown in Figure 2.

**Figure 2.** Kort nozzle (**a**), Becker Mewis Duct (**b**), and gate rudder system (**c**).

The foundation of a GRS is based on the originating activities, in Japan, to improve the maneuverability of coastal vessels which require tighter control of ships in their transverse motions at ports. This propulsion and maneuvering device was further developed by the recent R&D activities in the UK, e.g., Sasaki et al. (2015, 2018, 2017, 2019) [1,4–6]. The GRS was applied for the first time on a 2400 GT full-scale, new-built coastal container "Shigenobu", which was entered into service on November 2017. This was to demonstrate the vessel's performance, especially her excellent maneuverability performance. The comprehensive speed and maneuvering trials with this vessel and her sister ship "Sakura", indicated that the vessel with GRS was 14% more efficient at the design speed than her sister's while the gain in service can be as high as 30% in rough seas, as shown in Figure 3.

**Figure 3.** Powering performance comparisons of two sister ships, one with a gate rudder system and the other with a conventional flap-rudder system: In trials (**a**) and in-service (**b**).

The service performances of these sister ships, which operate on the same route and almost follow each other's path with the same mission in the northeast coast of Japan, are investigated based on the ship owner's standard logbook. This logbook continuously recorded the mean values of the important key performance indicators, such as ship speed, power, and fuel consumption for both vessels, since Nov 2017. As shown in Figures 3a and 4, the plot of the logbook data for powering and fuel consumption, respectively, indicates that the gain in performance for the ship with the GRS was as high as 30% or more than her sister ship with the conventional rudder system (CRS) [2,3].

**Figure 4.** In-service fuel consumption comparisons of two sister ships, Shigenobu with GRS (red) and Sakura with CRS (blue).

#### *1.2. Scale E*ff*ects*

While the main remarkable features of a GRS are highlighted in the previous section (Section 1.1), it should be asked "why did no one think of the GRS idea before?" One reason appears to be that the conventional modelling techniques are not suitable for use in an unconventional propeller-rudder configuration. It is not easy to say, but it strongly relates to the testing technology and the analysis procedures. A GRS is not within the scope of the existing model testing and scaling technology. For example, the resistance of the gate rudder measured in model tests was found to be rather high, i.e., 5 to 10 times as compared with the full scale due to the suspected scale effects. This gives the wrong conclusion for the model test results. In fact, the decision to apply a GRS in full scale was taken in Japan even though the model test results achieved from existing model testing methodologies were unsupportive and the full-scale performance was remarkably above the predicted gain based upon the model tests. The comparative result of the power prediction for the world's first gate rudder system driven ship, "Shigenobu", with the trials data using the combined ITTC and Yazaki method [7], can be seen in Figure 3. As shown in Figure 3a, on the one hand, the conventional prediction method did not present any gain for the gate rudder system while the full-scale trials of Shigenobu presented a 14% energy savings. On the other hand, as also shown in Figure 3a, the same method predicted the trial performance of her sistership "Sakura" with the conventional flap-rudder system very well by raising the question for ships with the GRS. In fact, this was the major motivation of this paper to explore the potential scale effects, which may be the reason for the discrepancy between the predictions and the full-scale data for Shigenobu.

The power prediction of ships based on model tests is one of the main tasks for a towing tank facility. Within this context, the conduct of tank tests and their analysis procedures have been historically developed by taking into account not only theoretical approaches but also empirical model-ship correlation factors to achieve the accurate full-scale power predictions at sea trial. In fact, the introduction of the turbulence stimulators is the most well-known practice of the towing tanks by artificially tripping the flow to be turbulent on the model hull surface. However, it is also a well-known fact that the laminar flow can be experienced over the appendages in the stern region, even within the thick boundary layers which can be stimulated for turbulent flow by the above-mentioned procedure of using a turbulence stimulator. It is also true that the turbulence stimulator is not applied to the models of the conventional rudders because they operate in the propeller slipstream with the accelerated flow which can suppress the presence of laminar flow and its separation, whereas this may not be true for the GRS driven models due their different arrangements as will be discussed later.

In this paper, the reason for the above-mentioned scale effect for the GRS driven ships is explored and verified by using the model test results of two different size models with the GRS. The aim is to take a further step towards an improved estimation of the powering performance of ships with the GRS. The scale effect is associated with the drag and lift characteristics of the gate rudder blades and correction procedures were proposed based on the semi-empirical approaches supported with the available model test and full-scale trials data. The suggested scale effect correction was also implemented in the powering performance prediction method for ships with the GRS and results were validated with the full-scale trials data for Shigenobu.

#### **2. Scale E**ff**ect Prediction for the Gate Rudder System**

#### *2.1. E*ff*ect of the Rudder Position*

As shown in Figure 1a, the gate rudder blades are located on either side of a propeller with large clearances. Therefore, the flow field surrounding the gate rudder is quite different from that of a conventional rudder case (Figure 1b) with the following distinct features:


The difference in the flow field between the model and full scale depends on the model size. If the model length (*LM*) is not large enough (i.e., *LM* < 12 m), the flow around the gate rudder blades has the possibility of being laminar and even developing a laminar flow separation because of their locations and that of the large thickness to chord ratio for the rudder blades. This is expected to result in the scale effect for the gate rudder blades. In fact, the scale effect of the rudder drag should be considered not only for the gate rudder but also for the conventional rudder. However, one can only appreciate the difference clearly if the comparisons of the flow characteristics are made based on the real case [5].

#### *2.2. Drag Coe*ffi*cients in Model and Full Scale*

The resistance of a rudder blade, FRX, and the side force (lift), FRY, can be represented by Equations (1) and (2) as follows:

$$F\_{\rm RX} = F\_{\rm RD} \cos(\alpha) - F\_{\rm RL} \sin(\alpha) \tag{1}$$

$$F\_{RY} = F\_{RD} \sin(a) + F\_{RL} \cos(a) \tag{2}$$

where, *FRD* and *FRL* is the contribution from the rudder drag and the rudder lift, respectively and α is the angle of attack of the rudder wing section to the flow. *FRL* is negligibly small for the conventional rudder case except for the condition behind a rotating propeller.

FRD can be predicted by the empirical formula given by Equation (3) when the flow velocity and rudder geometry is given.

$$F\_{RD} = \frac{1}{2} \rho \int\_0^H V\_o(z)^2 \mathcal{C}\_F(z) \ast \left( 1 + \frac{t(z)}{c(z)} + \left( \frac{t(z)}{c(z)} \right)^2 \right) \tag{3}$$

where *Vo* and *CF* are the local flow velocity and frictional resistance coefficient, respectively, corresponding to flow direction and flow characteristics (laminar or turbulent, etc.) at z position and t/c is the thickness-chord ratio in the same position.

Here, the drag coefficient of a rudder can be represented by Equation (4) using ship speed and rudder area *SR*.

$$C\_{RD} = \frac{F\_{RD}}{\frac{1}{2}\rho V\_S^2 S\_R} \tag{4}$$

It should also be noted that each of the resistance components obeys a different set of scaling laws and the problem of scaling can become more complicated because of the interaction between these components. Therefore, we explore the scale effect of the rudder drag by using data belonging to the gate rudder system of the Shigenobu, as described in the following:

Using Equation (3) the rudder drag was calculated for the gate rudder and the conventional rudder and results are presented as a comparison in Tables 2 and 3 for the model and full scale, respectively. The comparative results are also presented in Figure 5. The values in Figure 5 and Tables 2 and 3 are nondimensionalized by the measured ship resistance. To avoid confusion, it should be highlighted that the resultant rudder drag is different from these figures for the GRS because of the lift force acting on the rudder blades. The thrust (i.e., negative resistance) of gate rudder is quite often seen, even in the towing condition.

**Table 2.** Rudder drag calculations (in model scale).



**Table 3.** Rudder drag calculations (in full scale).

**Figure 5.** Rudder drag in % of ship resistance for model (**a**) and full scale (**b**).

As shown in Tables 2 and 3 and Figure 5, it is evident that the drag components of the two rudder cases are somewhat contrasting; the model scale drag of the gate rudder is six to eight times that of the conventional rudder, and both rudder drag components are decreased in full scale by a factor of one-third to one-quarter. Therefore, the scale effect of the gate rudder is relatively more significant as compared with that of the conventional rudder and the difference between the model and full-scale drag components of the gate rudder is 3.6% (5.3% minus 1.7%) of the ship resistance while it is only 0.6% (0.8% minus 0.2%) for the conventional rudder case. It is rather fortunate that the difference is six times, thanks to the flow speed difference around the rudder blades at each towing condition.

#### *2.3. Rudder Drag Correction for the Scale E*ff*ect*

As explained in Section 2.2, rudder drag cannot be measured directly during the resistance test of a hull with the gate rudder. This is because the blades of the gate rudder produce the lift force, and hence compensate for the rudder drag while a conventional rudder is simply a drag source contributing to the ship resistance. However, if we can measure the two rudder force components, FRX and FRY, in the ship fixed coordinate system, we can configure the rudder drag and lift components based on several assumptions within the wing theory. Hence, one can describe the lift coefficient as follows:

$$\mathbf{C}\_{L} = \kappa \left(\alpha + \alpha\_{\mathbb{X}}\right) \tag{5}$$

where *CL* is the lift coefficient, α and α*<sup>g</sup>* are attack angle and zero lift angle, respectively, and κ is the lift slope correction factor.

However, the rudder drag coefficient, CRD, and angle of attack, α, can be estimated by the following equations;

$$\mathbf{C}\_{RD} = \frac{F\_Y' - \mathbf{C}\_L \left[1 - \left(\alpha + \alpha\_\S\right)^2\right]^{0.5}}{\alpha + \alpha\_\S} \tag{6}$$

$$\alpha = \frac{\left(\kappa + F\_X'\right) - \sqrt{\left(\kappa + F\_X \nu\right)^2 + 2F\_Y \nu^2}}{-F\_Y'} - a\_\mathcal{S} \tag{7}$$

where, *FX* and *FY* is nondimensional rudder force of *FRX* and *FRY*, respectively and given by Equations (8) and (9) as follows:

$$F\_{X'} = \frac{F\_{RX}}{\frac{1}{2}\rho V\_S^2 S\_R} \tag{8}$$

$$F\_Y \prime = \frac{F\_{RY}}{\frac{1}{2}\rho V\_S^2 S\_R} \tag{9}$$

We can observe a positive flow angle, α, for every kind of vessel when the rudder blades are off-centered, as sketched in Figure 6.

The lift slope correction factor, κ, can be expressed by Equation (10) as follows:

$$\kappa = \varepsilon \frac{6.13\lambda}{2.25 + \lambda} \tag{10}$$

where λ is the aspect of ratio, ε is the effect of low Reynolds number on the lift slope which will be explained in Section 2.4. CL and CD can be obtained from the measured FX and FY during the resistance test directly.

**Figure 6.** Rudder forces originated from lift and drag.

If we can express the rudder drag coefficient by Equation (11) which is combined with the drag coefficient CRD0 explained earlier:

$$\mathcal{C}\_{RD} = \mathcal{C}\_{RD0} + \delta \mathcal{C}\_{RD} \tag{11}$$

where δ*CRD* represents the additional resistance due to the rudder stock. Conservatively, we can use this additional resistance component without correction (i.e., no scale effect) such as wave resistance. Hence the effect on the rudder resistance:

$$
\delta F\_{RX} = \frac{1}{2} \rho V\_S^2 \delta C\_{RD0} S\_R \cos \alpha \tag{12}
$$

$$
\delta \mathcal{C}\_{\text{RD0}} = \mathcal{C}\_{\text{RD0}\text{S}} - \mathcal{C}\_{\text{RD0}\text{M}} \tag{13}
$$

Figure 7 shows the difference between the obtained *CRD* and calculated *CRD*<sup>0</sup> (model). The δ*CRD0* is less than 1% of the total hull resistance, and the effect of this additional uncertain resistance on the full-scale performance is not as significant based on this figure.

**Figure 7.** Obtained rudder drag coefficients.

#### *2.4. Rudder Lift Correction for the Scale E*ff*ect*

The lift coefficient of the gate rudder is also influenced by the model scale effect, and hence requires correction of the model test data. For this correction, the wind tunnel test data of NACA0012 section in low Reynolds numbers with the nonlinear lift slope curves are used, as shown in Figure 8 from McCormick (1995) [8].

**Figure 8.** Effect of low Reynolds number on lift coefficients of typical wing section (NACA24xx series).

From Figure 8, the lift coefficient of the full-scale rudder (CLS) can be estimated by using Equation (14) in conjunction with Equations (5) and (10) as follows:

$$\varepsilon = \frac{1.470X\_M{}^3 - 3.109X\_M{}^2 + 2.376X\_M + 1.036}{1.470X\_S{}^3 - 3.109X\_S{}^2 + 2.376X\_S + 1.036} \tag{14}$$

if *RNS* <sup>&</sup>gt; <sup>8</sup> <sup>×</sup> <sup>10</sup>6, *XS* <sup>=</sup> <sup>8</sup> <sup>×</sup> 106 where

$$X\_M = R\_{NM} \times 10^{-7} \\ X\_S = R\_{NS} \times 10^{-7}$$

Figure 9 also shows the Reynolds number effect on the lift coefficients of other typical NACA wing sections presented by the same study [8].

**Figure 9.** Reynolds number effect on the lift coefficients of typical NACA wing sections.

In order to show the significance of the resultant forces acting on the rudder in the model and full scale, which are evaluated earlier, Figure 10 is included. As shown in Figure 10, the effects of the rudder drag and lift correction on the gate rudder performance are rather significant, and therefore this phenomena explains the discrepancy between the model test and the full-scale results. In the Shigenobu case, two rudder blades seem to be generating a thrust of almost more than 10%. Therefore, the earlier derived two corrections are essential to assess the actual performance of the gate rudder system, which need to be implemented in the powering performance prediction and is discussed in Section 4.

**Figure 10.** Effect of rudder drag and lift correction on rudder resultant force (model point case) to ship resistance.

#### **3. Verification of Scale E**ff**ect Correction by Model Tests**

In this section, the earlier proposed scale effect correction procedure is verified by the lift and drag coefficients of the gate rudder blades for two cargo ship models of different scales (2.0 m and 6.18 m long models). The verification is based on the data obtained from the resistance and self-propulsion tests of these models. Table 4 shows the principal dimensions of the cargo ship and its model size, and Figure 11 shows one of the models (6.18 m). Here, Lpp is the length between perpendiculars (m), B is the beam (m), d is the draft (m), and DP is the propeller diameter (m). Table 5 presents the test conditions of the two models.



**Table 5.** Model tests conducted with two scaled models.


**Figure 11.** Large (6.18 m) ship model tested in 400 m towing tank.

From the model tests conducted, as shown in Table 5, the following verification data can be obtained:


The verification data were calculated and are presented in Figure 12 in terms of the nondimensional drag and lift coefficients, (i.e., *CDR* and *CL*) of the rudders, as described earlier, using Equations (11) and (5), respectively. As shown in Figure 12, the proposed procedure shows good agreement with the two different scale model test data.

**Figure 12.** Gate rudder blades drag coefficient, *CDR*, (top) and lift coefficient, *CL*, (bottom) obtained with two different size models.

#### **4. Enhanced Procedure for Powering Performance Prediction**

Having established the scale-effect correction procedure in Section 2 and verified it with the model test data as described in Section 3, these corrections are introduced in the analysis of the resistance and self-propulsion test data to predict the powering performance of a ship with the gate rudder system in full scale as described in the following sections.

#### *4.1. E*ff*ective Power*

The effective horsepower (EHP) of a ship can be calculated based on the improved total resistance of the model by taking into account the scale effect correction on the rudder drag and rudder lift coefficients. Hence,

$$EHP = R\_{TS} \ V\_S \tag{15}$$

$$R\_{TS} = C\_{TS}0.5\rho V\_S^2 S \tag{16}$$

where *CTS* is the total resistance coefficient of the ship and is estimated based on the total model resistance coefficient according to the standard procedure, such as a recommended by the ITTC standard procedure.

Now, the total model resistance coefficient can be represented as:

$$\mathcal{C}\_{TM} = \frac{R\_{TM} + \delta F\_{RD} \cos \alpha + \delta F\_{RL} \sin \alpha}{0.5 \rho V^2 S\_R} \tag{17}$$

#### *4.2. Thrust Deduction Factor*

The scale effect correction on the thrust deduction factor to be obtained from the self-propulsion tests can be included by introducing the drag and lift correction on the rudder blades, as described in Sections 2.3 and 2.4, and implemented in Equation (18):

$$1 - t = \frac{R\_{TM} - F}{T + \delta F\_{RD} \cos \alpha + \delta F\_{RL} \sin \alpha} \tag{18}$$

#### *4.3. E*ff*ective Wake*

The effective wake of the GRS is the most difficult item to analyze since the propeller advance speed is also accelerated by the gate rudder blades and this effect is not be considered as an integral part of the effective wake, since the effective wake, by definition, is originated from the boundary layer deformation due to a propeller's suction effect as the function of the propeller's thrust. Therefore, the actual effective wake of the GRS is less than that of a conventional rudder system because the propeller thrust is smaller than that of the conventional configuration.

Bearing in mind the above fact, to define the wake fraction of the gate rudder system, we need the mean flow speed at the propeller plane that can be represented in the nondimensional form, *vP*, at the propeller plane of the gate rudder system, as in Equation (19):

$$
\upsilon\_P = \mathcal{C}\_1 \upsilon\_{A0} + \upsilon\_{\text{inP}} + \upsilon\_{\text{inR}} \tag{19}
$$

where *vA*0, *vinP* and *vinR* are the propeller advance speed of the conventional rudder case, the propeller self-induced velocity, and the rudder induced velocity, respectively.

*C*<sup>1</sup> is a correction factor of the wake variation to account for the difference in the propeller diameter and the position and recommended value for this *C*<sup>1</sup> is <1.0 because of the smaller propeller diameter, and hence the resulting thrust of the gate rudder propeller as compared with the conventional type.

Then, the wake fraction for the gate rudder can be written as follows:

$$w\_{GR} = C\_1 \* (w\_0 - 0.04) + w\_{inR} \tag{20}$$

where, *winR* is the rudder induced wake, as described earlier and its mean value can be estimated by the following formula:

$$w\_{inR} = C\_2 \ast C\_T + w\_{0R} \tag{21}$$

where *C2* is the correction factor for the thrust loading.

In Figure 13, a schematic representation of the scale effect for the gate rudder system is represented in comparison with the conventional rudder case. As shown in this figure, the dotted line presents the scale effect of a conventional rudder case, whereas the solid line shows the gate rudder case, respectively. One should also note in Figure 13 that, while point A' can be predicted from point A by using the ITTC recommended procedure, point B' cannot be predicted from point B which can be sometimes smaller, as shown in Figure 9, since point B' does not follow the same principle.

**Figure 13.** Schematic diagram of the scale effect of the wake of a gate rudder propulsion system.

Having represented the effective wake for the gate rudder system, Figure 14 is included to present the analysis results for Shigenobu (with GRS) and Sakura (with CRS-flap rudder) based on their respective sea trials and including the predicted results using the earlier described scale effects correction procedure.

**Figure 14.** Effect of drag and lift correction on predicted and measured (speed trials) effective wake.

#### *4.4. Powering Performance Prediction*

In order to present an enhanced procedure for the powering performance prediction of a ship with the GRS, including the earlier described scale effect corrections, an algorithm is presented in Figure 15 in terms of a flow chart.

Finally, the above-described procedure is applied to predict powering performance of the Shigenobu (GRS), and results are shown in Figure 16 as compared with the prediction results for the Sakura (CRS) and including the trials data for both ships [9]. As one can see in Figure 16, the predicted power for Shigenobu is in excellent agreement with the trials data and, hence, justify the scale effect corrections applied on the gate rudder drag and lift characteristics.

**Figure 15.** Algorithm for an enhanced powering performance procedure for a ship driven by a gate rudder system.

**Figure 16.** Comparison of trial power predictions for two ships using the ITTC and enhanced method for the gate rudder system.

It should be noted that the full-scale effective wake is estimated from the model test, and the same figures are used for the power prediction (*weS* = *weM*).

#### **5. Conclusions**

This study explored the scaling effect issues associated with the powering performance prediction of a ship fitted with a gate rudder system (GRS). The study aimed to take a further step towards a realistic estimation of the powering performance of ships with a GRS. The study focused on the corrections for the scale effects, which were believed to be associated with the drag and lift characteristics of the gate rudder blades due to the low Reynolds number experienced in model tests combined with the unique arrangement of this rudder and propulsion system. On the basis of the appropriate semi-empirical approaches and supporting model test and full-scale data, the study verified the scale effect phenomenon and presented the associated correction procedure. Together with this, the study also presented an enhanced procedure for the powering performance prediction of a ship driven by a gate rudder system implementing the proposed scale effect correction.

On the basis of the above, the following conclusions are obtained:


This study focused on a rapid and practical solution to the powering problem associated with a gate rudder system. However, this study would greatly benefit from further in-depth studies involving CFD, systematic model tests, and full-scale trials which are underway with the increasing applications of this new attractive energy-saving device, Tacar et al. (2019) [10].

**Author Contributions:** N.S. conducted the study; S.K. introduced the original gate rudder conceptualization; M.F. contributed to the application and validation of the conceptualization; M.A. contributed further advancement of the concept, review, and editing. All authors have read and agreed to the published version of the manuscript.

**Funding:** In this paper, the Shigenobu full-scale data was obtained from a research project supported by the Nippon Foundation, whereas, the model test data of the cargo ship was obtained from another research project supported by the subsidy for a demonstration project for energy efficiency in commercial transport sector introduced by the Ministry of Economy, Trade and Industry of Japan.

**Conflicts of Interest:** The authors declare no conflict of interests.

#### **References**


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