Turbulence cascade model for viscous vortex ring-tube reconnection

Abstract

The reconnection of a vortex ring and a vortex tube in a viscous fluid with the effects of two vortex core sizes (σ0=0.12r0 and 0.24r0, where r0 are initial ring radius) and three initial flow configurations (left-offset, center, and right-offset) at Reynolds number (ReΓ) of 10 000 was investigated using a high-order vortex-in-cell method combined with a large-eddy simulation model. For the left-offset case, a large part of the ring, slipping over the tube, associates with a small part of the tube to establish a new vortex ring, whereas the rest of the tube is reconnected by another part of the ring. For the center case, half of the ring joins with a part of the tube to construct an elliptical vortex ring while the rest connects because of viscosity. The reconnected ring and tube become more stable and are like the initial ones in the ultimate stage. For the right-offset case, both the ring and tube's reconnection occurs, and the reconnected elliptical vortex ring is rapidly distorted. The proportion of reconnected ring increases, and then this ring section loses its integrity, decaying into a complex cluster of various-scales vortex structures in different shapes. At σ0=0.12r0, the secondary vortex structures surrounding the tube and ring appear in three cases, while they are only observed for the center case at σ0=0.24r0. For three flow configurations and two vortex core sizes, after the reconnection, the energy cascade of the flow approaches a k−5/3 slope of Kolmogorov's similarity hypotheses and a k−3 slope in the ranges of wavenumbers (k) from 3 to 10 and from 10 to 40, respectively. The highest population of small-scale coherent vortex structures is observed for the right-offset, followed by the center and left-offset. In addition, a larger number of these structures was observed for a smaller core size. This validates that the mixing performance is the best at a small vortex core and in the right-offset configuration.

Low order modeling of dynamic stall using vortex particle method and dynamic mode decomposition

“…The particle core size is defined as 1/275 at Re =1000, as referred to references. 31,[48][49][50] As shown in Figure 3, the vorticity contours of the present results qualitatively agree well with those of reference for three angles of attack. In particular, the sizes of the leading-and trailing-edge vortices of the present work coincide with those of reference.…”

On the stability of a pair of vortex rings

“…2021), mixing from the interaction of a shock wave with a material interface (Zabusky 1999; Zhou 2017 a , b ; Wadas & Johnsen 2020) and turbulent transition (Zhou et al. 1999; Duong, Nguyen & Nguyen 2021; Yao & Hussain 2022). Understanding the dynamics of isolated or a small number of vortices is essential for successful operation of engineering applications in propulsion and energy generation (Saffman 1995) and elucidates naturally occurring flows involving, for example, jellyfish mobility (Dabiri 2009; Nawroth et al.…”

Vortex particle method with iterative Brinkman penalization for simulation of flow past sharp-shape bodies

“…There has been many vortex method researches leading to challenging applications in fluid dynamics, such as hydrodynamics, 5 flow mediated transport, 6 dynamics of rotorcrafts’ turbulent wake, 7 vertical axis wind turbines, 8 aeroacoustics, 9 free jet, 10 flow controls, 11 and vortex reconnection in viscous fluids. 12 In the Lagrangian vortex method, the velocity is computed using the unbounded Green’s function, namely Biot-Savart formulation. Since the formulation is direct summation of individual particles within the unbounded domain, the cost is polynomially increased to N2 operations, where N is the particle number.…”