Vortex interactions in a two side-by-side cylinder near-wake

2005 ◽  
Vol 26 (3) ◽  
pp. 362-377 ◽  
Author(s):  
Z.J. Wang ◽  
Y. Zhou
Author(s):  
Kajsa Warfvinge ◽  
L. Christoffer Johansson ◽  
Anders Hedenström

Hovering insects are divided into two categories: “normal” hoverers that moves the wing symmetrically in a horizontal stroke plane, and those with an inclined stroke plane. Normal hoverers have been suggested to support their weight during both down- and upstroke, shedding vortex rings each half stroke. Insects with an inclined stroke plane should, according to theory, produce flight forces only during downstroke, and only generate one set of vortices. The type of hovering is thus linked to the power required to hover. Previous efforts to characterize the wake of hovering insects have used low-resolution experimental techniques or simulated the flow using CFD, and so it remains to be determined if insect wakes can be represented by any of the suggested models. Here, we used tomographic PIV, with a horizontal measurement volume placed below the animals, to show that the wake shed by hovering hawkmoths are best be described as a series of bilateral, stacked vortex “rings”. While the upstroke is aerodynamically active, despite an inclined stroke plane, it produces weaker vortices than the downstroke. In addition, compared to the near wake, the far wake lacks structure and is less concentrated. Both near and far wakes are clearly affected by vortex interactions, suggesting caution is required when interpreting wake topologies. We also estimated induced power (Pind) from downwash velocities in the wake. Standard models predicted a Pind more than double that from our wake measurements. Our results thus question some model assumptions and we propose a reevaluation of the model parameters.


2021 ◽  
Vol 117 ◽  
pp. 102918
Author(s):  
Francisco Alves Pereira ◽  
Alessandro Capone ◽  
Fabio Di Felice

2014 ◽  
Vol 136 (3) ◽  
Author(s):  
C. Morton ◽  
S. Yarusevych

The turbulent wake development of a circular cylinder with a single stepwise discontinuity in diameter was investigated experimentally using flow visualization and two-component Laser Doppler Velocimetry (LDV). A single step cylinder is comprised of two cylinders of different diameters (D and d). Experiments were performed at a Reynolds number (ReD) of 1050 and a diameter ratio (D/d) of two. A combination of hydrogen bubble and laser induced fluorescence techniques allowed visualization of complex vortex dynamics in the near wake. The results show that turbulent vortex shedding from a single step cylinder occurs in three distinct cells of constant shedding frequency. The differences in frequency and strengths between vortices in the cells lead to complex vortex interactions at the cell boundaries. The results demonstrate that vortex splitting, half-loop vortex connections, and direct cross-boundary vortex connections occur near the cell boundaries. A comparative analysis of flow visualizations and velocity measurements is used to characterize the main vortex cells and the attendant vortex interactions, producing a simplified model of vortex dynamics in the step cylinder wake for ReD = 1050 and D/d = 2.


1997 ◽  
Vol 4 (3) ◽  
pp. 211-221 ◽  
Author(s):  
Alain Texier ◽  
Madeleine Coutanceau ◽  
Nathalie Boisaubert
Keyword(s):  

AIAA Journal ◽  
1997 ◽  
Vol 35 ◽  
pp. 1151-1163
Author(s):  
F. Grasso ◽  
S. Pirozzoli

Author(s):  
Elcilane Araújo de Freitas ◽  
Letícia Castelo Branco ◽  
Erick Oliveira do Nascimento ◽  
André Araujo ◽  
Erb Lins

Author(s):  
Suzane Nascimento ◽  
Juan Jose Cruz Villanueva ◽  
Luís Fernando Figueira da Silva

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