Laminar mixing of heterogeneous axisymmetric coaxial confined jets

AIAA Journal ◽  
1969 ◽  
Vol 7 (11) ◽  
pp. 2072-2078 ◽  
Author(s):  
KIRTI N. GHIA ◽  
T. PAUL TORDA ◽  
ZALMAN LAVAN
Keyword(s):  
1974 ◽  
Vol 13 (3) ◽  
pp. 184-190 ◽  
Author(s):  
Donald Bigg ◽  
Stanley Middleman

1970 ◽  
Vol 21 (4) ◽  
pp. 680-681
Author(s):  
Bernard Otterman ◽  
Shao-Lin Lee
Keyword(s):  

2019 ◽  
Vol 205 ◽  
pp. 25-35 ◽  
Author(s):  
Fan Zhang ◽  
Arnaud Erriguible ◽  
Samuel Marre

PAMM ◽  
2006 ◽  
Vol 6 (1) ◽  
pp. 527-528 ◽  
Author(s):  
Mirko Javurek ◽  
Raimund Wincor ◽  
Markus Brummayer

2012 ◽  
Vol 2012 ◽  
pp. 1-10 ◽  
Author(s):  
Koji Takahashi ◽  
Yoshiharu Sugo ◽  
Yasuyuki Takahata ◽  
Hitoshi Sekine ◽  
Masayuki Nakamura

The mixing performance in a vessel agitated by an impeller that inclined itself, which is considered one of the typical ways to promote mixing performance by the spatial chaotic mixing, has been investigated experimentally and numerically. The mixing time was measured by the decolorization method and it was found that the inclined impeller could reduce mixing time compared to that obtained by the vertically located impeller in laminar flow region. The effect of eccentric position of inclined impeller on mixing time was also studied and a significant reduction of mixing time was observed. To confirm the experimental results, the velocity profiles were calculated numerically and two novel numerical simulation methods were proposed.


2008 ◽  
Vol 47 (8) ◽  
pp. 1234-1245 ◽  
Author(s):  
M.T. Kandakure ◽  
V.C. Patkar ◽  
A.W. Patwardhan
Keyword(s):  

Author(s):  
Peter L. Woodfield ◽  
Kazuya Tatsumi ◽  
Kazuyoshi Nakabe ◽  
Kenjiro Suzuki

A three-dimensional unstructured finite-volume method is used to investigate laminar flow characteristics of a miniature chamber with a possible application to micro gas turbine combustor design. The chamber is cylindrical in shape and 20mm in diameter with the fuel stream entering via a single jet in the center of one end of the can. Oxidizer jets are generated by a circular baffle plate having six holes surrounding the fuel jet. Attention is given to the effect of the inlet conditions on the flow structure and mixing pattern inside the chamber. Computations are carried out with the calculation domain inlet being positioned at two different locations; (1) at the immediate entrance to the combustion chamber (2) one combustor diameter upstream of the baffle plate. Numerous inlet conditions are considered including ‘top-hat’, fully-developed, swirling, an annular backward facing step and some asymmetrically skewed profiles. The baffle plate is shown to have a significant smoothing effect on the inlet conditions for a Reynolds number of 100.


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