Intermittency of laminar separation bubble on a sphere during drag crisis

Abstract

The phenomenon of drag crisis for uniform flow past a smooth sphere is investigated via experiments in a low-turbulence wind tunnel for $1.5\times 10^{5}\leqslant Re\leqslant 5.0\times 10^{5}$. The Reynolds number, $Re$, is based on the free-stream speed and the diameter of the sphere. Based on the activity related to the laminar separation bubble (LSB), the critical regime for the occurrence of drag crisis ($3.4\times 10^{5}<Re<4.4\times 10^{5}$) is further divided into three subregimes. The gradual decrease of mean drag coefficient ($\overline{C}_{D}$) with $Re$, in subregime I, is due to the increase of base pressure and suction near the shoulder of the sphere. The flow is devoid of an LSB in this regime. The coefficient $\overline{C}_{D}$ decreases very rapidly with increase in $Re$ in subregime II primarily due to the increase in mean base pressure ($\overline{C}_{P,b}$). This subregime is characterized by intermittent switching of $C_{D}$ and $C_{P,b}$ between bistable states. Statistical analysis of the surface-pressure and force coefficients relates this behaviour to the intermittent appearance/disappearance of the LSB. The two states of the flow are referred to as the LSB and non-LSB states. The frequency of appearance of the LSB and the duration of its stay increase with increase in $Re$. An intermittency factor $I_{f}$, defined as the fraction of time during which the LSB exists in the flow, is estimated at each $Re$. The value of $I_{f}$ is zero in subregime I and increases from zero to one, with increase in $Re$, in subregime II. The variation of $\overline{C}_{D}$ with $Re$ is found to follow the variation of ($1-I_{f}$) with $Re$. This shows that the decrease of $\overline{C}_{D}$ with increase in $Re$, during drag crisis, is primarily due to the increased probability of the LSB state as opposed to the non-LSB state. A spatio-temporal analysis of the surface pressure measured at various polar locations on the surface of the sphere confirms the axisymmetric nature of the intermittent LSB. In subregime III of the critical regime, the LSB exists at all time instants ($I_{f}=1$). The $\overline{C}_{D}$ value continues to decrease with $Re$ in this subregime due to increase in $\overline{C}_{P,b}$. Unlike the general belief that the decrease in $\overline{C}_{D}$ with increase in $Re$ is due only to the increase in $\overline{C}_{P,b}$, it is found that the increase in suction upstream of the shoulder of the sphere, with increase in $Re$, also plays an important role. In particular, in the high subcritical regime ($2.5\times 10^{5}<Re<3.4\times 10^{5}$), the gradual decrease in $\overline{C}_{D}$ with increase in $Re$ is due solely to the increase in suction in a region upstream of the shoulder of the sphere.

Secondary vortex, laminar separation bubble and vortex shedding in flow past a low aspect ratio circular cylinder

“…A similar behaviour was reported by Deshpande et al. (2017) for the LSB on a sphere. In the subcritical regime, the SV is weak and as a result it does not cause significant variation in the surface distribution.…”

Investigation of Reverse Swing and Magnus Effect on a Cricket Ball Using Particle Image Velocimetry

“…The range of Reynolds numbers shown here corroborates with the critical regime for a sphere with a surface roughness of k/d = 250 × 10 −5 . The laminar separation bubble can be highly unsteady around the critical Reynolds number, as demonstrated by Deshpande et al [15]. Figure 10 shows two velocity "snapshots" at the same Re.…”

“…The laminar separation bubble can be highly unsteady around the critical Reynolds number, as demonstrated by Deshpande et al [15]. Figure 10 shows two velocity "snapshots" at the same Re.…”

“…Deshpande et al also showed that an LSB forms over the SS at low Re during the CS regime. Earlier experiments by Deshpande et al [15] demonstrated the instability and intermittency of an LSB over a smooth sphere, by means of unsteady force and pressure measurements. They found that the critical flow regime can be further categorized into three sub-regimes based on the nature of the LSB.…”

Scale Effects on Cavitation about a Sphere

“…After boundary layer transition (supercritical), the turbulent flow remains attached further around the sphere, reducing the width of the wake and thus reducing the drag. The flow state is complicated further by the presence of a laminar separation bubble which intermittently exists near the Reynolds number transition [9] and is ever-present for Re > 375 × 10 3 .…”