Experimental investigation on the leading-edge vortex formation and detachment mechanism of a pitching and plunging plate

2020 ◽  
Vol 901 ◽  
Author(s):  
Zhen-Yao Li ◽  
Li-Hao Feng ◽  
Johannes Kissing ◽  
Cameron Tropea ◽  
Jin-Jun Wang
Keyword(s):  
Experimental Investigation ◽  
Vortex Formation ◽  
Leading Edge ◽  
Leading Edge Vortex ◽  
Edge Vortex ◽  
Image Position

Abstract

scholarly journals Video: Leading edge vortex formation in aquatic swimming

2014 ◽  
Author(s):  
Mohsen Daghooghi ◽  
Richard G. Bottom ◽  
Iman Borazjani
Keyword(s):  
Vortex Formation ◽  
Leading Edge ◽  
Leading Edge Vortex ◽  
Edge Vortex

Initiation of Leading-Edge-Vortex Formation on Finite Wings in Unsteady Flow

2015 ◽  
Author(s):  
Yoshikazu Hirato ◽  
Minao Shen ◽  
Sachin Aggarwal ◽  
Ashok Gopalarathnam ◽  
Jack R. Edwards
Keyword(s):  
Unsteady Flow ◽  
Vortex Formation ◽  
Leading Edge ◽  
Leading Edge Vortex ◽  
Edge Vortex

Effects of Reynolds number on leading-edge vortex formation dynamics and stability in revolving wings

2021 ◽  
Vol 931 ◽  
Author(s):  
Long Chen ◽  
Luyao Wang ◽  
Chao Zhou ◽  
Jianghao Wu ◽  
Bo Cheng
Keyword(s):  
Reynolds Number ◽  
Steady State ◽  
Numerical Methods ◽  
Vortex Formation ◽  
Leading Edge ◽  
Leading Edge Vortex ◽  
Formation Dynamics ◽  
Edge Vortex ◽  
Vorticity Balance ◽  
Vortex Compression

The mechanisms of leading-edge vortex (LEV) formation and its stable attachment to revolving wings depend highly on Reynolds number ( $\textit {Re}$ ). In this study, using numerical methods, we examined the $\textit {Re}$ dependence of LEV formation dynamics and stability on revolving wings with $\textit {Re}$ ranging from 10 to 5000. Our results show that the duration of the LEV formation period and its steady-state intensity both reduce significantly as $\textit {Re}$ decreases from 1000 to 10. Moreover, the primary mechanisms contributing to LEV stability can vary at different $\textit {Re}$ levels. At $\textit {Re} <200$ , the LEV stability is mainly driven by viscous diffusion. At $200<\textit {Re} <1000$ , the LEV is maintained by two distinct vortex-tilting-based mechanisms, i.e. the planetary vorticity tilting and the radial–tangential vorticity balance. At $\textit {Re}>1000$ , the radial–tangential vorticity balance becomes the primary contributor to LEV stability, in addition to secondary contributions from tip-ward vorticity convection, vortex compression and planetary vorticity tilting. It is further shown that the regions of tip-ward vorticity convection and tip-ward pressure gradient almost overlap at high $\textit {Re}$ . In addition, the contribution of planetary vorticity tilting in LEV stability is $\textit {Re}$ -independent. This work provides novel insights into the various mechanisms, in particular those of vortex tilting, in driving the LEV formation and stability on low- $\textit {Re}$ revolving wings.

Optimal Leading Edge Vortex Formation of a Flapping Foil in Energy Harvesting Regime

2017 ◽  
Author(s):  
Firas F. Siala ◽  
Alexander D. Totpal ◽  
James A. Liburdy
Keyword(s):  
Energy Harvesting ◽  
Vortex Formation ◽  
Leading Edge ◽  
Flux Analysis ◽  
Leading Edge Vortex ◽  
Flapping Foil ◽  
Flow Energy ◽  
Edge Vortex ◽  
Formation Number ◽  
Harvesting Regime

An experimental investigation is conducted to study the leading edge vortex (LEV) evolution of a simultaneously heaving and pitching foil operating in the energy harvesting regime. Two dimensional particle image velocimetry measurements are collected in a wind tunnel at reduced frequencies of k = fc/U = 0.05–0.20. Vorticity flux analysis is performed to calculate the constant C in the vortex formation number equation proposed by J. O. Dabiri [1], and it is shown that for a flapping foil operating in the energy harvesting regime, this constant is approximately equal to 1.33. We demonstrate that the optimal LEV formation number (T̂max ≈ 4) is achieved at k = 0.11, which is well within the range of optimal reduced frequency for energy harvesting applications (k = 0.1–0.15). This suggests that the flow energy extraction is closely related to the efficient evolution process of the LEV.

3D Effects in the Wake Vortex Formation of an Elliptic Flat Plate in Hover

2017 ◽  
Author(s):  
Vivek Nair ◽  
Siddarth Chintamani ◽  
B. H. Dennis
Keyword(s):  
Flat Plate ◽  
Vortex Formation ◽  
Three Dimensional ◽  
Leading Edge ◽  
Leading Edge Vortex ◽  
Elliptic Geometry ◽  
3D Effects ◽  
Edge Vortex ◽  
Formation Number ◽  
Vorticity Transport

A Numerical Analysis is conducted to investigate the Leading Edge Vortex (LEV) dynamics of an elliptic flat plate undergoing 2 dimensional symmetric flapping motion in hover. The plate is modeled with an aspect ratio of 3 and a flapping trajectory resulting in Reynolds number 225 is studied. The leading edge vortex stability is analyzed as a function of the non dimensional formation number and a vorticity transport analysis is carried to understand the flux budgets present. The LEV formation number is found to be 2.6. The results of vorticity analysis show the highly three dimensional nature of the LEV growth for an elliptic geometry.

Leading Edge Vortex Formation on Finite Wings Using Vortex Particles

2021 ◽  
Author(s):  
Hugh J. Bird ◽  
Kiran Kumar Ramesh ◽  
Shuji Otomo ◽  
Ignazio Maria Viola
Keyword(s):  
Vortex Formation ◽  
Leading Edge ◽  
Leading Edge Vortex ◽  
Edge Vortex
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