IMPINGEMENT OF AN UNDEREXPANDED SONIC JET ON A CYLINDRICAL BODY

1999 ◽  
Vol 6 (2) ◽  
pp. 105-114
Author(s):  
Hideo Kashimura ◽  
Tsuyoshi Yasunobu ◽  
Manabu Takao ◽  
Toshiaki Setoguchi
Keyword(s):  
Author(s):  
Johan Roenby ◽  
Hassan Aref

The model of body–vortex interactions, where the fluid flow is planar, ideal and unbounded, and the vortex is a point vortex, is studied. The body may have a constant circulation around it. The governing equations for the general case of a freely moving body of arbitrary shape and mass density and an arbitrary number of point vortices are presented. The case of a body and a single vortex is then investigated numerically in detail. In this paper, the body is a homogeneous, elliptical cylinder. For large body–vortex separations, the system behaves much like a vortex pair regardless of body shape. The case of a circle is integrable. As the body is made slightly elliptic, a chaotic region grows from an unstable relative equilibrium of the circle-vortex case. The case of a cylindrical body of any shape moving in fluid otherwise at rest is also integrable. A second transition to chaos arises from the limit between rocking and tumbling motion of the body known in this case. In both instances, the chaos may be detected both in the body motion and in the vortex motion. The effect of increasing body mass at a fixed body shape is to damp the chaos.


2021 ◽  
Vol 71 ◽  
pp. 104449
Author(s):  
Vahid Foroughi ◽  
Adriana Palacios ◽  
Carlos Barraza ◽  
Alba Àgueda ◽  
Christian Mata ◽  
...  
Keyword(s):  

2020 ◽  
Vol 0 (0) ◽  
Author(s):  
Arun Prasad R ◽  
Thanigaiarasu S ◽  
Sembaruthi M ◽  
Rathakrishnan E

AbstractThe present numerical study is to understand the effect of air tabs located at the exit of a convergent nozzle on the spreading and mixing characteristics of correctly expanded sonic primary jet. Air tabs used in this study are two secondary jets issuing from constant diameter tubes located diametrically opposite at the periphery of the primary nozzle exit, normal to the primary jet. Two air tabs of Mach numbers 1.0 to 1.4, in steps of 0.1 are considered in this study. The mixing modification caused by air tabs are analysed by considering the mixing of uncontrolled (free) primary jet as a reference. Substantial enhancement in jet mixing is achieved with Mach 1.4 air tabs, which results in 80 % potential core length reduction. The total pressure profiles taken on the plane (YZ) normal to the primary jet axis, at various locations along the primary jet centreline revealed the modification of the jet cross sectional shape by air tabs. The stream-wise vortices and bifurcation of the primary jet caused by air tabs are found to be the mechanism behind the enhanced jet mixing.


1981 ◽  
Vol 113 (-1) ◽  
pp. 299 ◽  
Author(s):  
J. Iwamoto ◽  
B. E. L. Deckker
Keyword(s):  

1994 ◽  
Vol 20 (1) ◽  
pp. 31-41 ◽  
Author(s):  
Francisco J. Romay ◽  
Benjamin Y. H. Liu ◽  
David Y. H. Pui

2013 ◽  
Vol 25 (2) ◽  
pp. 196-204 ◽  
Author(s):  
Hua-wei Zhou ◽  
Hong-sheng Zhang

2002 ◽  
Vol 16 (11) ◽  
pp. 1448-1456 ◽  
Author(s):  
Heuy-Dong Kim ◽  
Hideo Kashimura ◽  
Toshiaki Setoguchi
Keyword(s):  

2021 ◽  
Author(s):  
Edward Lee ◽  
You Huang ◽  
Bojan Vukasinovic ◽  
Ari Glezer

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