Asymmetric vortex pair in the wake of a circular cylinder

AIAA Journal ◽  
1994 ◽  
Vol 32 (10) ◽  
pp. 1999-2003 ◽  
Author(s):  
G. Iosilevskii ◽  
A. Seginer
2021 ◽  
Vol 33 (12) ◽  
pp. 125115
Author(s):  
Zhicheng Wang ◽  
Ang Li ◽  
Baiheng Wu ◽  
Dixia Fan ◽  
Michael S. Triantafyllou ◽  
...  

2014 ◽  
Vol 9 (3) ◽  
pp. JFST0050-JFST0050 ◽  
Author(s):  
Shunsuke FUNAOKA ◽  
Shunsuke YAMADA ◽  
Seiji ICHIKAWA ◽  
Hitoshi ISHIKAWA

2006 ◽  
Vol 13 (6) ◽  
pp. 641-649 ◽  
Author(s):  
B. Cariteau ◽  
J.-B. Flór

Abstract. We investigate the elliptical instability of a strongly asymmetric vortex pair in a stratified fluid, generated by the acceleration and deceleration of the rotation of a single flap. The dominant parameter is the Froude number, Fr=U/(NR), based on the maximum azimuthal velocity, U, and corresponding radius, R, of the strongest vortex, i.e. the principal vortex, and buoyancy frequency N. For Fr>1, both vortices are elliptically unstable while the instability is suppressed for Fr<1. In an asymmetric vortex pair, the principal vortex is less – and the secondary vortex more – elliptical than the vortices in an equivalent symmetric dipolar vortex. The far more unstable secondary vortex interacts with the principal vortex and increases the strain on the latter, thus increasing its ellipticity and its instability growth rate. The nonlinear interactions render the elliptical instability more relevant. An asymmetric dipole can be more unstable than an equivalent symmetric dipole. Further, the wavelength of the instability is shown to be a function of the Froude number for strong stratifications corresponding to small Froude numbers, whereas it remains constant in the limit of a homogenous fluid.


2010 ◽  
Vol 24 (13) ◽  
pp. 1405-1408 ◽  
Author(s):  
ZIJIE ZHAO ◽  
CHAO GAO ◽  
FENG LIU ◽  
SHIJUN LUO

Forward blowing from a pair of plasma actuators on the leeward surface and near the apex is used to switch the asymmetric vortex pair over a cone of semi-apex angle 10° at high angles of attack. Wind tunnel pressure measurements show that by appropriate design of the actuators and appropriate choice of the AC voltage and frequency, side forces and yawing moments of opposite signs can be obtained at a given angle of attack by activating one of the plasma actuators. Further work is suggested.


1989 ◽  
Vol 9 (Supplement) ◽  
pp. 23-26
Author(s):  
Hideo YAMADA ◽  
Atsushi ITOH ◽  
Haruo YAMABE ◽  
Toshiyuki GOTOH

1986 ◽  
Vol 23 (2) ◽  
pp. 136-140
Author(s):  
Takashi Abe ◽  
Katushi Funabiki

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