3.1. Analysis of the CFD Calculation Results
Figure 7 shows time-averaged axial velocity contours on the symmetrical plane of the computational domain. As it can be observed, the channel expanded between 0–35
H, which led to an adverse pressure gradient (APG), and a continuous decrease in fluid velocity. Under the action of the APG and wall viscosity, flow separation occurred at the lower wall, and a low-velocity zone appeared. The flow separation position was approximately at
x1 ≈ 20
H. Since the free-slip wall boundary condition was adopted on the upper wall of the computational domain, no flow separation occurred. In the 35–135
H section, there was a zero pressure gradient (ZPG), and flow reattachment occurred at
x2 ≈ 60
H. The axial velocity contours with VGs revealed that the VGs inhibited flow separation in all four cases. When the VG spacing was
λ/
H = 7, a small low-speed region appeared at
x ≈ 30
H. When the VGs spacing was
λ/
H = 9, the area of the low-speed region at the same location increased. This showed that when
λ/
H = 9, the effectiveness of the concentrated vortices at this location became weak, while the hydrodynamic energy was already low under the inverse pressure gradient due to the large spacing between VGs. No low-velocity zone appeared at the other two installations with a smaller spacing.
Figure 8 shows the distribution of the pressure coefficient (
Cp) on the bottom wall of the computational domain. In the no VG case, the inflection point of
Cp appeared at
x ≈ 20
H, and the slope of the
Cp change decreased. In the cases where the boundary layer flow was controlled by the VGs, the
Cp on the wall increased in the APG section. Since no flow separation occurred, no alteration in the slope of
Cp change in the APG section was observed. The
Cp in most positions of the ZPG segment was basically 0. The difference between different VG spacings was primarily reflected in the turning position of the
Cp curve. In particular, the larger the VG spacing, the smaller the slope of the wall pressure drop and the worse the flow control effect. After the fluid passed through the expansion section, the
Cp increased. According to
Figure 7, the flow separation occurred at
x ≈ 20
H. After the flow separation, the slope of the
Cp drop decreased, while after the flow reattachment, no significant changes in
Cp were observed in the ZPG section.
Although in some simple flows, the existence of vortices can be determined by intuition and visualization, in three-dimensional viscous flows, especially in complex flows, a large number of experimental or numerical simulation data are required to show the structure, evolution, and interaction of vortices. Therefore, it is necessary to give an objective discrimination of the vortices’ criteria. At present, the
Q criterion is more commonly used, where the region of
Q > 0 is defined as a vortex, that is
. Its physical meaning is that the fluid rotation in the region of the vortex plays a leading role in comparing the strain rate. The specific formula is as follows:
where
and
,
,
are the strain rate tensor and the vorticity tensor, respectively.
In this study, the Q criterion was used to identify the three-dimensional vortices in the flow field.
Figure 9 shows the
Q isosurfaces colored according to the velocity in the flow field (
Q = 1 × 10
5). Many disordered vortices were observed in the turbulent flow field without VGs. However, typical turbulent coherent structures could be distinguished. In the initial flow stage, under the fluid viscosity and shear stress, the vortices were rolled up near the wall (as indicated by A). Due to self-rotation of the vortices, the radius of the vortex cores increased gradually downstream. At the same time, disturbed by the three-dimensional flow field, the vortices fluctuated extensively, twisted, and protruded upward along the normal direction. The protrusion was induced by the self-rotation of the spanning vortices, which intensified the protrusion height (as indicated by B). Under the action of a shear flow, the vortices continued to stretch and lift, and gradually developed into closed upper end hairpin vortices with an opening at the lower end (as indicated by C). Moving backwards, the legs of the vortices extended and the head of the hairpin vortices became larger, forming a local high-shear layer. Under the action of the mainstream fluid, the vortex was stretched along the flow direction into a tube (as indicated by D). This indicated that in turbulent flows, the average length of the vortex tube was generally increased. The energy transport process from larger to smaller vortices and the viscous dissipation into heat is called the cascade principle.
Figure 10 shows
Q isosurfaces colored according to the velocity in the flow field (
Q = 1 × 10
5) as a result of the VG control. First, by comparing
Figure 9 and
Figure 10, it can be found that without the VG control, many irregular vortices were generated downstream of the computational domain, while this number was reduced when the flow was controlled by VGs. By comparing the vortices under different VG spacings, it can be found that with the increase of the VG spacing, the height of the vortices increased. As it can be seen in
Figure 10b, the presence of VGs created longitudinal vortices, and this fact organized the local vortex structure and further hindered the development and movement of the spanwise vortices. The vortices generated between two VGs rotated in opposite directions, thus the outward vortices of the VGs were “suppressed.” On the other hand, the upward forces at the inner side of the VGs were toward the center. Under the action of the two concentrated vortices, the inner extended vortices were “raised” to form hairpin-like vortices, and as the flow developed downstream, the concentrated vortices gradually merged with the leg of the hairpin-like vortices. The legs of the concentrated and hairpin-like vortices played an important role in the exchange of kinetic energy and energy dissipation near the wall. When
λ/
H = 3, the centralized vortices generated by the two VGs were so close to each other that the spanning vortices inside the VGs were not “raised,” but instead were fused together at a downstream location under a reverse pressure gradient, forming hairpin-like vortices. When
λ/
H = 5, the outer spreading vortices of the VGs were “suppressed,” while the inner spreading vortices were “raised,” forming regular hairpin-like vortices that moved downstream. When
λ/
H = 7 and
λ/
H = 9, no regular hairpin-like vortices were developed on the inner side due to the large VG spacing. Such disordered turbulent structures were not conducive to the energy exchange in the near-wall region, which became prone to flow separation.
Figure 11 shows vorticity isolines and spatial streamlines at five cross-sectional locations downstream of the VGs. First, as it can be seen in
Figure 11a, the concentrated vortices generated by the VGs scrolled around the vortex core center and rotated in spirals. When
λ/
H = 7, at
x > 20
H, the streamlines began to bend due to the counter-pressure gradient effect, and the flow became unsmooth. When
λ/
H = 9, at
x > 20
H, the streamlines were twisted, which indicated that the VGs were not able to adequately suppress the flow separation. In
Figure 11b, it can be observed that with the increase of the VG spacing, the distance between the two vortices gradually increased. Downstream of
x/
H = 15, when
λ/
H = 7 and
λ/
H = 9, the shape of the vortices was irregular with no obvious vortex center, while the area surrounding the vortices increased. When
λ/
H = 3 and
λ/
H = 5, the two vortices were closer to each other, and the shape of the concentrated vortices was still intact. Since the concentrated vortices rotated upward at the inner side of the VGs and were subjected to upward forces, the highest vortex core height from the wall was observed at
λ/
H = 3. When the distance between the vortices was small enough, the upward rotation force made the vortices lift off the wall. This implies that in order to restrain the flow separation using VGs, the vortices need to be closer to the wall to give a stronger energy exchange effect in the near-wall area, and the more beneficial the flow control. When
λ/
H = 3, the spacing was somewhat small, which was not conducive to flow control.
Figure 12 shows the relationship between the vortex core radius and vortex core spacing with flow distance, where
r represents the vortex radius and
Δz represents the distance between the two vortex cores. With the increase of the VG spacing, the
Δz increased gradually. The vortex core radius represents the radial range of action. Theoretically, when VGs are used to suppress flow separation, the optimal distance is when the vortex radius
r is equal to the distance between the two vortex cores
Δz/2 (half the distance). However, the radius of the vortices increased along the flow direction, and the vortices slightly deviated toward the flow direction. Therefore, the radius of the vortices and spacing between vortices cannot be equal everywhere along the flow direction. When the distance between vortices was
Δz/2 <
r, VGs hindered the development of vortices. When
Δz/2 >
r, a region where the vortices could not act was developed, which led to the decrease of the added value of fluid kinetic energy in the boundary layer. By comparing the four different VG spacing results, it can be seen that, except at
x/
H = 1, the distance between the vortices
Δz was smaller than the vortex radius
r at the other locations when
λ/
H = 3. This shows that this VG spacing hindered the development of vortices at most positions along the flow direction, and that the VG spacing was too small to facilitate flow control. When
λ/
H = 7 and 9,
Δz >
r for each direction, which reduced the effective range of the vortices and was not conducive to flow control. When
λ/
H = 5, it was found that
Δz >
r before
x/
H = 10, while after
x/
H = 10,
Δz <
r. Consequently, a VG spacing of
λ/
H = 5 was more suitable for flow control.
Second-order spatial correlation is a statistical method commonly used to study turbulence. Two-point spatial correlation can reflect the spatial relationship of one or more pulsations in the turbulent flow field. This method can be used to analyze the correlation of the structural characteristics of the downstream VG vortices. The correlation function is defined as follows:
where
ui and
uj are components of the pulsating velocity, and
x and
r are vectors. When
i =
j, this expresses the autocorrelation of a certain pulsation, and when
i ≠
j, it means that the two pulsations are correlated. The autocorrelation diagram is shown in
Figure 13.
The above formula can be transformed into dimensionless correlation coefficients as follows:
The correlation coefficient magnitude represents the statistical similarity between two random variables or the probability that the fluctuation takes the same sign at different positions in the flow field. denotes that two random variables are completely correlated, while denotes that they are completely unrelated. For uniform turbulence, the correlation coefficient is independent of the coordinate position, and related only to the correlation distance. In order to investigate the correlation of the turbulent momentum downstream of the VGs, the correlation characteristics of the turbulent momentum v′ along the flow direction at certain points at different heights on a pair of centrosymmetric planes of the VGs were compared.
Figure 14 illustrates the autocorrelation coefficient curve
for the calculation of the fluctuating velocity
v′ at different positions on the central symmetry plane of the domain. Five reference points at different heights and different points along the flow direction were selected for coherence analysis (
Figure 14a). The minimum correlation distance was 0.5 mm, the maximum correlation distance was 675 mm, and the VGs were placed at the 0 position. According to
Figure 14b, the coherence coefficient at the reference point is 1, indicating that the reference point was correlated with itself. In addition, the larger the correlation coefficient near the reference point, the larger the correlation coefficient amplitude, and the higher the correlation between the fluctuation and the reference point. A comparison between the following four cases demonstrated that when
λ/
H = 3, the magnitude of the correlation coefficient was the largest at most locations, which indicated that at this VG spacing, the structure of turbulence in the downstream domain preserved a high organization. When
λ/
H = 7 and 9, the magnitude of the correlation coefficient was larger at most locations, while that of
λ/
H = 5 was closer to
at most locations. The correlation between the turbulent vortices downstream of the VGs and the reference point was poor, indicating that this VG spacing (
λ/
H = 5) was more suitable for suppressing flow separation. The width between the correlation coefficient curve and the two intersections reflected the scale of the coherent structure in the downstream turbulent flow field. It can be observed that the scale of the vortices increased gradually as the flow developed downstream.
Figure 15 shows the average velocity distribution at different positions along the downstream direction. <
u>/
U∞ represents the ratio of the time-averaged velocity to the mainstream velocity and
y/
H is the ratio of the normal wall height to the VG height. It can be observed that the increase in the kinetic energy of the fluid at the bottom of the boundary layer corresponded to a decrease in the kinetic energy of the fluid above the boundary layer. The S-type velocity profile took the center of the vortex core as the symmetrical point, which is the main principle of using VGs to control flow separation. In particular, due to the rotation of the concentrated vortices, the high-energy fluid outside of the boundary layer was transferred into the bottom of the boundary layer, inhibiting the boundary layer separation. By comparing the velocity profiles developed under the four VG spacings, it can be seen that the kinetic energy of the fluid at the bottom of the boundary layer increased with the decrease of the VG spacing. However, when
λ/
H = 3, downstream of
x/
H = 15, the center of the vortex core was higher than the wall, and the high-energy fluid in the boundary layer was also higher than the wall height. When
λ/
H = 5, the kinetic energy at the bottom of the boundary layer was the largest.
Figure 16 shows the relationship between the pressure loss coefficient
CΔP and the VG spacing. The percentage decrease of
CΔP with VGs compared to that without VGs (clean) can be observed. When VGs were installed, the
CΔP in the calculation domain decreased compared to that without VGs. Among them, the
CΔP was the smallest when
λ/
H = 5, and the maximum
CΔP was reduced by 30.95%. When
λ/
H = 9, the
CΔP was the largest, which was reduced by 2.37% compared to that without VGs. Therefore,
λ/
H = 5 was more suitable for flow control.
3.2. Analysis of the Experimental Results
Figure 17 shows the lift–drag coefficient and lift–drag ratio curves of the airfoil with and without VGs.
Figure 17a demonstrates the lift coefficient curve. It can be seen that the lift coefficients of the airfoil with and without VGs were almost the same for an angle-of-attack (AoA) below 8°. Above 8°, the VGs could effectively increase the lift of the airfoil. In
Table 4, it can be seen that when
λ/
H = 9, the stall AoA of the airfoil was 16°, while under the other VG spacings, the stall AoA was 18°. The maximum lift coefficient was obtained when
λ/
H = 5, which was increased by 48.77% compared to that of the clean airfoil. When
λ/
H = 3,
λ/
H = 7, and
λ/
H = 9, the maximum lift coefficient increased by 45.67%, 48.32%, and 30.20%, respectively. Therefore, the maximum lift coefficient of the airfoil was the largest when
λ/
H = 5. On the other hand, the drag coefficient was the worst when
λ/
H = 9. In
Table 3, it can be seen that when
λ/
H = 3, the drag coefficient of the airfoil decreased by 82.06% compared to that of the clean airfoil at an AoA of 18°. In addition, it decreased by 83.28% when
λ/
H = 5, by 78.43% when
λ/
H = 7, and by 13.06% when
λ/
H = 9. The lift–drag ratio of the airfoil increased by 741.03% compared to that of the clean airfoil at an AoA of 18° when
λ/
H = 3, by 821.86% when
λ/
H = 5, by 612.06% when
λ/
H = 7, and by 55.06% when
λ/
H = 9.
In
Figure 18, the surface pressure coefficient (
Cp) distribution of the airfoil is presented. It can be seen that the curves of
Cp distribution on the airfoil surface with and without VGs coincided at 0° and 5° AoA. At AoAs of 10°, 15°, and 18°, the VGs postponed the pressure plateau to some extent. However, when
λ/
H = 9, the effect of the VGs flow control was the worst, and the pressure plateau appeared earlier than in the other three cases. It can be observed that the
Cp curves of the other three VG spacings basically coincided. At an AoA of 20°, the
Cp curves and the position of the pressure platform of
λ/
H = 9 were similar to those of the clean airfoil, while the
Cp curves of the other three VGs spacings were similar. At 22°, the
Cp curves of
λ/
H = 3 and
λ/
H = 5 basically coincided with the clean airfoil, while
λ/
H = 7 exhibited the best effect. When the AoA was equal to 25°, the
Cp curves of the airfoil with VGs coincided with those of the clean airfoil.
Figure 19 shows the curve of the total pressure coefficient distribution at the wake rake. It can be seen that at AoAs of
α = 0°, 5°, and 10°, for an airfoil with VGs, the total pressure loss at the wake rake was larger because the generators increased the thickness of the boundary layer and thus increased the viscous losses. When the AoA was 15° and 18°, the total pressure loss of the airfoil with VGs was smaller than that of the clean airfoil. Among the four VG spacings, the total pressure loss of the airfoil with VGs was the largest when
λ/
H = 9, and under the other three spacings, the total pressure loss was similar. At
α = 20°, the total pressure loss was the largest when
λ/
H = 9 and the smallest when
λ/
H = 7. At
α = 22°, the total pressure loss was the largest when
λ/
H = 7, which was larger than that of the clean airfoil, while the total pressure loss of
λ/
H = 7 was the smallest. When
α = 25°, the total pressure loss was the same, with or without VGs.