2.2. Numerical Setup
In CFD simulations, the Reynolds-Averaged Navier–Stokes (RANS) equations are among the most widely applied approaches. The detailed methodologies and governing equations for numerical modeling have been extensively described in previous studies [
1,
3,
6,
7,
13,
14,
15]. In CFD simulations, each step of the modeling process can significantly influence the accuracy and reliability of the results. These include the definition of the computational domain, the mesh structure and refinement level, the boundary conditions, and the turbulence model adopted. Therefore, every stage of the simulation setup, as well as the selection of computational parameters, should be carried out based on well-established guidelines and validated through previous modeling experience [
16,
17,
18].
The turbulence model plays a particularly important role, especially for flows characterized by separation, strong vortices, or complex distributions of turbulent kinetic energy. Due to computational constraints, it is impractical to directly resolve all turbulence scales through Direct Numerical Simulation (DNS) for engineering-scale problems. Hence, Reynolds-Averaged Navier–Stokes (RANS) models such as
k–
ε,
k–
ω, or
SST are commonly employed to represent the mean effects of turbulence on the flow field [
14,
16,
17,
19]. The selection of the turbulence model has a direct impact on the predicted velocity and pressure distributions, as well as on drag and lift forces. Each turbulence model is based on different assumptions concerning the production, dissipation, and transport of turbulent kinetic energy, leading to variations in the prediction of flow separation, recirculation zones, and near-wall velocity gradients [
2,
13,
16,
20,
21].
In this research, the aerodynamic performances of the ship are analyzed using the commercial CFD package ANSYS Fluent v.19.2, employing the
k–
ε turbulence viscous model for unsteady flow [
19,
21,
22]. The velocity inlet is given at the inlet as the wind velocity, and the pressure outlet is given at the outlet of the computed domain. The bottom, top, and sides are assessed at the walls. The computational domain was defined with dimensions of 6.5 L in length, L in width, and L in height, where L denotes the ship length. For this research, with an actual ship length of 43.25 m, the domain dimensions were determined as 200 m in length, 40 m in width, and 40 m in height. The domain was discretized using an unstructured mesh consisting of approximately 2.683 million cells.
Boundary conditions were imposed corresponding to wind velocities ranging from Beaufort level 1 to level 5, which represent Reynolds numbers between 6 × 10
6 and 2.2 × 10
7. The detailed input parameters are summarized in
Table 2, and
Figure 3 illustrates the computational domain and the mesh configuration.
In CFD simulations, each step of the modeling process can significantly influence the results. To obtain reliable results, all stages of the computation must strictly follow validated guidelines and best practices documented in authoritative references [
2,
5,
7,
11,
20,
23,
24,
25,
26]. Moreover, the accuracy of numerical predictions can be verified by comparing the simulation results with experimental model tests or benchmark data from recognized studies. Grid convergence assessment, together with prior experience in applying CFD to similar problems, also serves as an important approach to evaluate the reliability of the simulation results [
2,
3,
4,
11,
15,
27,
28].
In this study, a mesh convergence analysis was conducted using seven different mesh numbers, with corresponding
y+ values ranging from 4.786 to 128.262. The simulations were carried out under identical boundary conditions, with a flow velocity corresponding to a Reynolds number of
Rn = 6.26 × 10
6.
Table 3 and
Figure 4 present the comparison of wind drag acting on the ship for the different mesh configurations. The results confirm that the selected mesh provides sufficient numerical accuracy and stability for the CFD simulations.
In the calculation, the wind drag coefficient is defined as follows:
where
Cd is the total wind drag coefficient acting on the ship
Rd is the total wind drag acting on the ship, N;
Cd(f) is the component of the frictional viscous wind drag;
Cd(p) is the component of the pressure viscous wind drag;
V is the velocity of the ship, m/s.
The comparison of wind drag coefficients acting on the ship, as illustrated in
Figure 4, indicates that the deviation resulting from varying the mesh density in the investigated region remains below 2.63%. As the
y+ value decreases, the deviation is significantly reduced, reaching below 0.5%. These results confirm the mesh convergence and provide a reliable basis for the subsequent numerical simulations conducted in this study.
The CFD results have been thoroughly validated in numerous published studies, demonstrating their accuracy and robustness in predicting flow fields, pressure distributions, and wind drag acting on the ships. These validations provide a strong basis for employing CFD in the present study to investigate the aerodynamic performance and wind drag acting on the ships [
1,
2,
3,
5,
7,
10,
11,
22,
23,
24,
26].
In our previous study, the validation of CFD results was performed for the same problem. The CFD results of wind drag acting on several model ships named as Chip Carrier were investigated by comparing with those of the experimental results at the towing tank [
2,
11].
Figure 5 shows the results of the comparison between CFD and experimental results of the wind drag coefficient acting on the Chip Carrier model at a Reynolds number of 12 × 10
6. In the CFD results, the turbulent viscous model
k–
ε for unsteady flow was used, and a mesh was generated in the computed domain with 3.8 million unstructured elements. The value of the
y+ was from 15 to 50 in the different computed cases. The results show fairly good agreement between the CFD and experimental data.
2.3. Results of Aerodynamic Performance Acting on the Original River Cargo Ship
Based on the calculation of the aerodynamic performances of the original model,
Figure 6 shows the results of the pressure distribution around the hull and wind drag acting on the ship in the different Reynolds numbers. The pressure distribution around and over the hull surface of the ships shows that the bow shape and the accommodation have higher-pressure areas than other areas. Thus, the concentration of pressure areas occurs in areas with large and sharply changing wind surfaces on the hull. These are the areas that may need to be improved in design to reduce the area of this high-pressure area. The pressure exerted on the hull causes wind drag, so it is essential to reduce the areas of high pressure during the ship’s design process. In addition, it is possible to change the ship’s operating posture or adjust the wind direction acting on the ship to control and change the areas of high pressure acting on the ship, helping to reduce the wind drag acting on the ship.
Figure 7 shows that as the velocity increases, the wind drag coefficient acting on the ship tends to decrease. In the velocity range corresponding to Reynolds numbers below 18.6 × 10
6, the wind drag coefficient acting on the hull tends to stabilize and change less than when the velocity increases beyond the Reynolds limit of 18.6 × 10
6. The results of wind drag acting on the ship surveyed above are consistent with the CFD calculation results obtained on the pressure distribution and flow around the ship, as shown.
Table 4 shows the detailed wind drag acting on the ship.
The observed decrease in the drag coefficient with increasing flow velocity, as shown in
Figure 7 and
Table 4, can be physically explained by the change in the relative contributions of form pressure wind drag, and friction wind drag as the Reynolds number increases. At higher velocities, the boundary layer becomes more turbulent, leading to delayed flow separation and a reduction in the wake region behind the body. Consequently, the form pressure wind drag component decreases more significantly than the slight increase in frictional wind drag, resulting in an overall reduction in total wind drag coefficient acting on the ship.