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ISSN : 1229-3431(Print)
ISSN : 2287-3341(Online)
Journal of the Korean Society of Marine Environment and Safety Vol.29 No.6 pp.672-680
DOI : https://doi.org/10.7837/kosomes.2023.29.6.672

Study of Small Craft Resistance under Different Loading Conditions using Model Test and Numerical Simulations

Jun-Taek Lim*, Michael**, Nam-Kyun Im***, Kwang-Cheol Seo****
*Graduate School of Mokpo National Maritime University, Mokpo 58628, Korea
**Graduate School of Mokpo National Maritime University, Mokpo 58628, Korea
***Professor, Department of Navigation Science, Mokpo National Maritime University, Mokpo 58628, Korea
****Professor, Department of Naval Architecture & Ocean Engineering, Mokpo National Maritime University, Mokpo 58628, Korea

* First Author : lognhorn15@gmail.com


Corresponding Author : kcseo@mmu.ac.kr, 061-240-7303
September 20, 2023 October 24, 2023 October 27, 2023

Abstract


Weight is a critical factor in the ship design process given that it has a substantial impact on the hydrodynamic performance of ships. Typically, ships are optimally designed for specific conditions with a fixed draft and displacement. However, in reality, weight and draft can vary within a certain range owing to operational activities, such as fuel consumption, ballast adjustments, and loading conditions . Therefore, we investigated how resistance changes under three different loading conditions, namely overload, design-load, and lightship, for small craft, using both model experiments and numerical simulations. Additionally, we examined the sensitivity of weight changes to resistance to enhance the performance of ships, ultimately reducing power requirements in support of the International Maritime Organization's (IMO) goal of reducing CO2 emissions by 50% by 2050. We found that weight changes have a more significant impact at low Froude Numbers. Operating under overload conditions, which correspond to a 5% increase in draft and an 11.1% increase in displacement, can lead to a relatively substantial increase in total resistance, up to 15.97% and 14.31% in towing tests and CFD simulations, respectively.



모형시험과 수치해석을 이용한 하중조건 변화에 따른 소형선박의 저항성능 변화에 관한 연구

임 준택*, 마 이클**, 임 남균***, 서 광철****
*목포해양대학교 대학원
**목포해양대학교 대학원
***목포해양대학교 항해학부 교수
****목포해양대학교 조선해양공학과 교수

초록


선박의 설계과정에 있어, 선박의 중량은 유체역학적 성능에 큰 영향을 미치는 가장 중요한 요소 중 하나이다. 선박은 일반적으 로 최적의 흘수와 배수량을 갖는 하나의 조건으로 설계되지만, 실제로는 연료의 소비, 선박 평형수의 충전과 적재 조건과 같은 운항 활동 으로 인해 선박의 중량 및 흘수가 일정 범위 내에서 바뀐다. 본 연구에서는 소형선박을 대상으로 3가지 하중조건에 따른 선박의 저항성능 변화를 모형실험과 수치해석을 통해 연구하였다. 마지막으로 2050년까지 CO2 배출 가스를 50% 감축한다는 국제해사기구(IMO) 목표를 따 라 선박의 저항 성능을 개선하여 동력 요구 사항을 줄이기 위해 선박의 중량 변화에 따른 저항성능의 민감도를 연구하였다. 연구 결과, 선박의 중량변화에 따른 효과는 낮은 프루드 수에서 크게 나타나는 것으로 확인되며, 저항성능에 대한 연구 결과, 설계 흘수의 적재조건 을 기준으로 배수량이 11.1% 증가하고, 흘수가 5% 증가한 Over load의 적재조건에서 운항 시 선체의 총 저항이 모형시험과 CFD 시뮬레이 션에서 각각 15.97%, 14.31%까지 증가하는 것을 볼 수 있다.



    1. Introduction

    Ships are designed to complete and answer the requirements of the ship’s owner, which can be concluded into one single operation scheme. This kind of philosophy causes a ship to be designed into one optimum condition to answer the purpose of the ship’s presence. During the design process, weight and displacement are the most important factors to consider. A ship’s main particulars are mainly chosen to be able to carry the weight or load within its limited working environment. This logic brings optimum ship characteristics such as length, breadth, height, and draught. Unlike other ship characteristics, draught is one of the parameters that is constantly changing due to many factors, such as fluid density, loading conditions, fuel consumption, stability problems, trim optimization, etc. Loading conditions are one of the factors that are unavoidable due to their natural changes during the operation. These changes mainly affect the ship’s draught which is sensitively changing the ship’s displacement, resulting in significant changes to the ship’s hydrodynamic performance, such as resistance.

    Many studies have been done to give a deeper understanding of this issue. A full-scale bulk carrier resistance assessment under different draughts is performed both using numerical and experimental studies (Farkas et al., 2018). Three different draughts are evaluated within various trim conditions on a container ship, aiming for an optimum condition in the actual navigation to reduce the ship’s resistance by the CFD method which is later experimentally verified (Gao et al., 2019). A prediction of container ship resistance under different draught is also studied with Radial Basis Function Neural Network (RBFNN) and other machine learning models (Yang et al., 2021). In confined waters, a vessel’s trim and draught are optimized to enhance the resistance characteristics of the KCS model using CFD (Campbell et al., 2022). Different displacement conditions of a planing catamaran are investigated by experimental and numerical methods to give a better understanding of the hydrodynamics of the vessel (Wang et al., 2022). Furthermore, the added resistance of a tanker in head waves for 4 different draughts is also studied experimentally and numerically. (Park et al., 2016).

    Most of the recent studies are focused on the relatively big size of ships or displacement vessels, which commonly happens due to the natural behavior of loading conditions changing during its operation. However, draught changes on small ships (< 499 GT) are commonly designed for semi-planing to the planing regime has a relatively big impact on its hydrodynamic performance.

    For the relatively small size of ships, a simple empirical formula is provided to predict the planing hull resistance (Savitsky, 1964) where displacement plays a significant role by maintaining the equilibrium moment of weight and hydrodynamic lift. Several studies of resistance performance analysis to support the design modernization of small-size vessels, especially fishing boats are also widely explored (Kim and Lee, 1984) (Lee, 1984) (Lee et al., 2006) (Kang et al., 2007) (Yu and Lee, 2007). Also, small crafts are numerically studied under low-speed (Jee et al., 2009) and high-speed (Yu et al., 2011) to see the resistance performance.

    Since it dominates up to 46% of the whole population of ships in the world (Equasis, 2020), this study aims to give a deeper understanding of the relationship between the loading conditions to the small craft’s resistance. In conclusion, an improvement could be made to have a lower power requirement to reduce CO2 gas emissions by up to 50% in alignment with the International Maritime Organization (IMO) goals for 2050 (IMO, 2018).

    2. Methodology

    In this study, three different speeds are analyzed under three different loading conditions. The study is performed both experimentally and numerically. The experimental analysis is performed in a high-speed towing tank facility under calm water conditions, while the numerical analysis is performed by a commercial Computational Fluid Dynamics (CFD) software of Simcenter Star-CCM+.

    2.1 Target Vessel

    A V-type planing hull form of a small craft with a 20-degree deadrise angle is used in this study. With the limitation of the towing tank facility, a final length of 1.972 m corresponding to a 1:9 scale is chosen. For the design load conditions, the ship’s model has a 31.325 kg displacement with 0.116 m draught. At the stern section, an improvement to increase the inflow to the propeller region is made by using a flat-roof tunnel stern, while a center keel is used in the centerline for stability. A linesplan of the small craft used as the target vessel is shown in Fig 1.

    2.2 Study Cases

    The changes in loading conditions are made by changing the draught of the targeted vessel while maintaining other parameters to be fixed. Three loading conditions of overload, design load, and lightship are made by changing the vessel’s draught (T) ranging from 0.96T to 1.05T, which is shown in Fig. 2.

    The resistance evaluation is made within the range of Froude Number of 0.56 – 0.91 to see the effect of each loading condition within the semi-planing to planing speed range. Therefore, a total of 3 different loading conditions were performed at 3 different speeds resulting in a total of 9 cases which are summarized in Table 2. Where draught is defined as T which is mentioned in Table 1, and CWP is the waterplane area coefficient. The waterplane area coefficients are within the range of 0.742 – 0.755, which is varied due to the changes in the bow section. With a relatively uniform stern section, there are no significant changes in waterplane form in the stern area. By increasing the vessel’s draught up to 5%, an overload condition with an 11% increase in displacement is achieved, while reducing the draught by 4% or corresponding to the lightship condition, a reduction of 9.4% displacement is achieved.

    3. Model Test Experiment

    A 1.972 m long small craft model is made with glass-fiber material, with foam composite for the construction. Five transverse frames and a deck edge ring frame are equipped to support the transverse and torsional stiffness. Thin mylar strips which are shown in Fig. 3, are added to the chine region to maintain the edge sharpness, which can separate the transverse flow. Additionally, solid wood mounting pads are installed as the measuring instrumentation seating, and two ballast weight pads are to support the changes in the ship’s loading conditions. The weight is equally distributed along the ship model to maintain the center of gravity. The model setup is presented in Fig. 4 below.

    3.1 Towing Tank Conditions and Measurement

    The towing test experiment is conducted in the high-speed towing tank 3 at the Davidson Laboratory, which is 95 m long by 5 m wide, and 2 m deep. The towing test facility is equipped with an electric motor with steel cable driven located above the center of the water tank. The towing carriage rides the monorail while the model is free to heave and pitch but fixed in other degrees of motion. The towing test experiments are performed for all cases with the towing test conditions as summarized in Table 3 below, as aligned with the ITTC guidelines and procedures to ensure the reliability of the test results (ITTC, 2014a) (ITTC, 2021).

    The instrumentations for resistance measurement are calibrated with the ITTC procedure (ITTC, 2017) before being used in the experiments. LVDT-based linear drag balance instruments are used for resistance evaluation, while the trim and speed are measured by Schaevitz-type linear servo inclinometer and linear quadrature encoder or PC-based clock, respectively. An absolute reading difference of 0.09 N for drag and 0.06 degrees for trim is recorded, which can be concluded as tolerable, and the device is well-calibrated and the towing test experiments are ready to be performed.

    3.2 Model Test Results

    The towing test experiments are performed for all considered cases. The total resistance is measured and summarized in Table 4. Along with the displacement and draught reduction, the resistance is reduced. This is easily known by the reduction length of waterline as shown in Fig. 2, which also reduced the wetted surface area.

    In Froude Number 0.56, changing load conditions from design load to overload condition gives a significant increase in resistance of up to 15.97%, while getting lower by up to 10.39% at Froude Number 0.91. Also, the resistance is greatly reduced by up to 11.07% by operating in lightship condition compared to the design load at the Froude Number 0.56 and reduced up to 9.27% at the Froude Number 0.91 for equivalent loading condition changes.

    The trend of resistance changes under different loading conditions is presented in Fig. 5. Loading conditions play an important role in every speed regime. Gives a significant increment of 10.39% - 15.97% by operating in an overload condition, and a reduction of 9.27% - 11.07% by operating in a lightship condition.

    4. Numerical Analysis

    Computational Fluid Dynamics (CFD) is a fluid mechanic-based software that can perform fluid flow problems with numerical analysis. In this study, commercial CFD software Simcenter Star-CCM+ is used to perform the analysis. CFD analysis is commonly used since it could capture the flow analysis better, and the sensitivity could be used to accommodate small changes in the ship design process with relatively less computational time compared to the towing test method.

    4.1 Methodology

    In recent studies, several methods are usually used for planing ship resistance evaluation, which targets the accuracy of the simulations. Reynolds-averaged Navier-Stokes (RANS) equations are commonly used as the governing equations for the viscous fluids within a time function in a finite volume, which can be seen in the equations below.

    d V d t + S ( t ) d S · ( u υ ) = 0
    (5)

    d d t V ( t ) u d V = S ( t ) d S · T ¯
    (6)

    T ¯ = ( u υ ) u P I ¯ + υ [ u + ( u ) T ]
    (7)

    Where dV is the volume element, t is the time, S(t) is the surface area vector, dS is a surface area element, u is the velocity vector, and v is the surface element velocity resulting from the motion of volume control. T is the stress tensor, P is the pressure, and -I is the identity tensor, ∇u is the gradient of u and superscript (.)T is the matrix transpose operator (Rosenfeld and Kwak, 1991).

    To simulate the turbulence flow characteristics, a modified turbulence model of SST-k-ω is used (Menter, 1994). This model could provide better accuracy at the boundary layer. The equations are presented as follows:

    D ρ k D t = τ i j δ u i δ x j β * ρ ω k + δ δ x j [ ( μ + σ ω μ t ) δ ω δ x j ]
    (8)

    D ρ ω D t = ϒ υ t τ i j δ u i δ x j β ρ ω 2 + δ δ x j [ ( μ + σ ω μ t ) δ ω δ x j ] + 2 ρ ( 1 F 1 ) σ ω 2 1 ω δ k δ x j δ ω δ x j
    (9)

    This turbulence model is derived by transforming the standard model of high-Reynolds-number k-ε to a k-ω turbulence model by applying multiplier blending factor of F1 or (1-F1). Several constants which used in this turbulence models are σk1 = 0.5, σw1 = 0.5, β1 = 0.075, β* = 0.09, κ = 0.41, σk2 = 1.0, σw2 = 0.856, β2 = 0.0828, γ 1 = β 1 / β * σ w 1 κ 2 / β * , γ 2 = β 2 / β * σ w 2 κ 2 / β * .

    To get the real condition of ship operation, the ship experiences resistance from multiphase fluids, namely water, and air. The free-surface area is defined as the region where the air and fluids are met, which in this case is the small craft’s draught. The complexity of this free surface is captured with High-Resolution Interface Capturing (HRIC), while the fluids are modeled using the multiphase model included in the CFD package. The volume of Fluid (VOF) is used to divide the heavy and light fluid of water and air by a volume fraction, between the range of 0 to 1 (0 < F < 1) .

    The loading conditions are simulated by changing several settings in the physics setup. First, the flat volume of the fluid wave (flat VOF wave) is used to model calm water conditions. The draught changes are applied by changing the point of the water level. Second, the displacement changes are set in the Dynamic Fluid Body Interaction (DFBI) settings, where the hull is set into a 3D continuum body, and the mass could be adjusted under this setting, along with the moment of inertia of the hull. The physics setup and configuration used in this study are listed in Table 5.

    For validation and verification, a recent study of a planing ship (Begovic and Bertorello, 2012) is used. This study provides the hull geometry along with the towing test result. In this process, the Warped-2 hull form is chosen among the hull forms. The Warped-2 hull form is a single chine v-type hull form which is chosen since it has relatively similar characteristics to the target vessel. With a length of 1.900 m, breadth of 0.424 m, and draught of 0.110 m, a displacement of 32.630 kg is achieved.

    The verification process is performed at 4 different speeds and the results are shown in Fig. 6, where the total resistance and is chosen as the parameter for the comparison, respectively. An average difference of 5.80% of total resistance is occurred. Considering the reasonable results, the same physic setup will be applied to the small craft as the target vessel.

    4.2 Computational Domain and Boundaries

    To reduce the computational time, the towing test is designed as small as possible but still large enough to capture the flow, and to avoid the reverse flow into the domain. Therefore, International Towing Tank Conference (ITTC) procedures and guidelines (ITTC, 2014b) are taken into consideration. The computational domain and boundaries is presented in Fig. 7 below.

    The numerical analysis is performed for a half section of the vessel port-side since it will give similar results for the starboard side. This method could reduce the computational time by reducing the number of cells, which can be done by applying symmetry plane boundaries in the ship’s geometry centerline. Followed by velocity inlet for the inlet, side, bottom, and top regions, and pressure outlet for the outlet regions. The hull geometry is set to wall regions, with overset boundaries made around the hull.

    4.3 Mesh Configurations

    The mesh configuration is one of the factors that need to be considered in the numerical simulations. In this study, overset mesh is used to reduce the number of cells in the simulations. Overset region is an adaptive meshing strategy that consists of donor cells and adaptor cells, which create a continuous layer by transforming information from cell to cell. Prism layer mesh is used around the boundary layer of hull regions with all y+ treatment methods, with a value of greater than 40 (y+ > 40). Richardson’s extrapolation (Richardson, 1927) is used to consider the optimum mesh size. Three sizes of meshes are considered, and finally resulting a mesh consisting of 2.57 million cells is created along with the volume control for the free surface and wake region refinement.

    4.4 Numerical Simulation Results

    The CFD analyses are performed for all considered cases, and the results are summarized in Table 6 below. The results are reasonably satisfactory since it has the same trend as the towing test results. A potential total resistance reduction of up to 11.28% was achieved at Froude Number 0.56, and 8.49% at Froude Number 0.91, by changing load conditions from design load to lightship.

    The trend of resistance changes under different loading conditions is presented in Fig. 8. The trend is similar to the towing test experiments which are previously done. Gives a significant increment of 10.94% - 14.31% by operating in an overload condition.

    5. Results and Discussion

    Both analyses are performed based on the guidelines and present studies for both experimental and numerical analysis. The results show a similar trend for all considered cases. Within all test conditions, CFD analyses always underperformed compared to the towing test experiment. As summarized in Table 7, a maximum difference of -2.625% while as close as a -0.361% difference was achieved between the CFD analysis and towing test experiment. Therefore, the CFD results are reliable and could be used to perform further analysis during the design process.

    In a higher Froude Number of 0.91, the difference gap tends to get wider compared to the lower Froude Number of 0.56. This phenomenon could be described as a Numerical Ventilation (NV) problem due to mesh sensitivity and the time-step of the simulation. This leads to a reduction in friction resistance which results in lower total resistance.

    The resistance evaluation is considered reasonably satisfactory and well simulates the towing test experiment as shown in Fig. 9. The resistance measured by both methods gives a similar trend. While the towing test method could capture the resistance increment of 15.97% at the low Froude Number of 0.56, the CFD results show similar results of 14.31%. Not only giving the same trend of increment, total resistance is reduced by up to 11.07% by the towing test method, and the CFD simulations of up to 11.28% for the same condition, proving that CFD simulations are considered reliable to perform further analysis. Giving a maximum resistance trend differences of 1.66% and as close as 0.20%.

    The resistance changes are more sensitive in lower Froude Number and could be theoretically proven. The fact that most of the resistance consists of frictional resistance which is mainly affected by the wetted surface area. Operating in the low-speed regime of Froude Number 0.56 tends to give a smaller hydrodynamic lift. With the absence of a hydrodynamic lift, the displacement of the vessel is dominant, and the bow is not sufficiently lifted, resulting in a longer length of waterline and a bigger wetted surface area. Therefore, in conclusion, by reducing the displacement by changing loading conditions in this speed regime, the resistance which mainly depends on the displacement could be highly reduced. While in the higher speed regime, a hydrodynamic lift is significantly produced, resulting in a shorter waterline and smaller wetted surface area. The displacement is greatly supported by the hydrodynamic lift, therefore, reducing the displacement will not affect as much as in low Froude Number.

    6. Conclusion

    This study concludes the effect of changing loading conditions on small craft resistance by towing test and CFD simulations. The total resistance of CFD simulations is underperformed compared to the towing tests, ranging from 0.36% – 2.63% less than towing test method. While comparing the trend of resistance changes, a maximum of 1.66% while as close as 0.20% is shown at the low Froude Number of 0.56. These results are considered satisfactory and the CFD simulations are reliable for further study.

    The weight sensitivity is more dominant in the lower Froude Number of 0.56 compared to the higher Froude Number of 0.91. Operating in an overload condition, or corresponding to an increase of the draught by 5%, could result in 11.1% more displacement, and could add as high as 15.97% to the total resistance. The same phenomenon also happened by operating in a lightship. Reducing the draught by 4.3%, resulting in a 9.4% reduction of displacement, could reduce the resistance to up to 11.07%.

    These happened due to the fact that in the low Froude Number, displacement plays a big role in the hydrodynamic performance since the hydrodynamic lift is lowly produced. Therefore, a greater wetted surface area and longer length of waterline is achieved. While in the higher Froude Number, the displacement is mainly supported by the hydrodynamic lift. Therefore, reducing the displacement in this speed regime gives a relatively smaller change to the hydrodynamic performance, compared to the lower Froude Number.

    A wider speed range and hull-form type are to be considered in further study. Due to limitations of time, only several loading conditions under specific hull-types and speeds are considered in this study. However, in fact, the potential of resistance changes under different loading conditions may vary between each hull form. In addition, the potential of loading conditions under different longitudinal centers of gravity (LCG) are also to be considered in the future due to the complexity of the equilibrium moment of weight acting on the center of gravity (CG) and hydrodynamic lift acting on the center of buoyancy (CB).

    Acknowledgment

    This research was supported by a grant (20015029) of Regional Customized Disaster-Safety R&D Program, funded by Ministry of Interior and Safety (MOIS, Korea).

    Figure

    KOSOMES-29-6-672_F1.gif

    Target vessel’s linesplan.

    KOSOMES-29-6-672_F2.gif

    Draught changes under different loading conditions.

    KOSOMES-29-6-672_F3.gif

    Mylar strips at the chine region.

    KOSOMES-29-6-672_F4.gif

    Towing test experiment model setup.

    KOSOMES-29-6-672_F5.gif

    Total resistance measured by towing test experiments.

    KOSOMES-29-6-672_F6.gif

    Total resistance comparison of Warped - Hull 2.

    KOSOMES-29-6-672_F7.gif

    Computational domain and boundaries.

    KOSOMES-29-6-672_F8.gif

    Total resistance measured by CFD simulations.

    KOSOMES-29-6-672_F9.gif

    Towing test (top), and CFD simulations (bottom) of small planing ship at design load in Froude Number 0.91.

    Table

    Full scale and model scale of the small craft main particulars at design load

    Small craft under different loading conditions

    Towing tank facility conditions

    Total resistance changes under different loading conditions measured by towing test experiments

    Physics setup

    Total resistance changes under different loading conditions measured by CFD simulations

    Total resistance changes under different loading conditions by towing test experiment and computational fluid dynamics (CFD)

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