Experimental study of a heterogeneous plasma flow in a reactor with a multijet mixing chamber

1997 ◽  
Vol 70 (4) ◽  
pp. 559-566
Author(s):  
V. D. Shimanovich ◽  
A. L. Mossé ◽  
L. E. Krat'ko ◽  
N. I. Chubrik ◽  
E. A. Ershov-Pavlov ◽  
...  
Keyword(s):  
Experimental Study ◽  
Plasma Flow ◽  
Mixing Chamber

Experimental Study of the Interaction of a Laser Plasma Flow with a Transverse Magnetic Field

2021 ◽  
Author(s):  
A. A. Soloviev ◽  
K. F. Burdonov ◽  
A. V. Kotov ◽  
S. E. Perevalov ◽  
R. S. Zemskov ◽  
...  
Keyword(s):  
Magnetic Field ◽  
Experimental Study ◽  
Transverse Magnetic Field ◽  
Plasma Flow ◽  
Laser Plasma ◽  
Transverse Magnetic

Experimental Study of Plasma Flow Control on Highly Swept Delta Wing

AIAA Journal ◽  
2010 ◽  
Vol 48 (1) ◽  
pp. 249-252 ◽  
Author(s):  
P. F. Zhang ◽  
J. J. Wang ◽  
L. H. Feng ◽  
G. B. Wang
Keyword(s):  
Experimental Study ◽  
Flow Control ◽  
Plasma Flow ◽  
Delta Wing ◽  
Plasma Flow Control

scholarly journals Experimental study of neoclassical plasma flow and bootstrap current in the tokamak TEXTOR

1994 ◽  
Vol 34 (11) ◽  
pp. 1461-1472 ◽  
Author(s):  
K Hothker ◽  
H.-J Belitz ◽  
R.P Schorn ◽  
W Bieger ◽  
J.A Boedo
Keyword(s):  
Experimental Study ◽  
Plasma Flow ◽  
Bootstrap Current

Experimental Study on Drag Enhancement in Electrodynamic Heat Shield for a Blunt Body in a Weakly Ionized Plasma Flow

2007 ◽  
Author(s):  
Masaaki Kawamura ◽  
Atsushi Matsuda ◽  
Hiroshi Katsurayama ◽  
Hirotaka Otsu ◽  
Detlev Konigorski ◽  
...  
Keyword(s):  
Experimental Study ◽  
Plasma Flow ◽  
Blunt Body ◽  
Heat Shield ◽  
Weakly Ionized ◽  
Weakly Ionized Plasma

scholarly journals Effect of Strut Geometry in Supersonic Mixing

2020 ◽  
Vol 9 (6) ◽  
pp. 386-389
Keyword(s):  
Experimental Study ◽  
Mach Number ◽  
Residence Time ◽  
High Speed ◽  
Free Stream ◽  
Mixing Enhancement ◽  
Supersonic Mixing ◽  
Mixing Chamber ◽  
Mixing Method ◽  
Selection Of

Effective mixing in a short mixing chamber is a major challenge in supersonic air breathing engines, especially the mixing between two high speed co-axial streams. The residence time is a major factor to get the two streams properly mixed. The selection of mixing method is crucial in the supersonic conditions. An experimental study has been performed on the supersonic mixing of air from strut injectors of various combinations in their trailing ramp angles with a free stream air of Mach number 2. Two different configurations of geometries, a plain geometry and a lobed geometry considered and further two different combinations, slot and hole injections, are taken for the study in each geometry. Among different combinations, it is found that a better mixing enhancement is achieved for the 9o lobed geometry struts.

scholarly journals Experimental Study on Internal Mixing Sonic Flow Air Assist Atomizer for Heavy Oils

1990 ◽  
Author(s):  
Ju Shan Chin ◽  
Li Xing Wang
Keyword(s):  
Experimental Study ◽  
Flame Length ◽  
Chamber Pressure ◽  
Heavy Oils ◽  
Air Supply ◽  
Air Stream ◽  
Internal Mixing ◽  
Mixing Chamber ◽  
Fine Spray ◽  
Sonic Flow

Based on the experiences previously obtained from the experimental study of plain jet atomization under cross flowing air stream and under supersonic air flow, the authors designed and studied a serious of internal mixing sonic flow air assist atomizers for heavy oil application. The contradiction between the requirements for fine spray (for high combustion completeness) and for long flame (for flame rigidity) often existing in industrial furnace has been solved. Good data were obtained which can be used for the design of such kind atomizers. By properly choosing the configuration and geometrical dimensions of the atomizer, also by choosing suitable values for mixing chamber pressure, air–liquid ratio, it is possible to have very fine spray and desirable flame length. The results showed that the ratio of mixing chamber pressure to air supply pressure should be in the range of 0.6 to 0.7. For atmospheric pressure combustion furnace, such air assist atomizer needs 0.4 MPa compressed air to have sonic flow at nozzle exit. This type of air assist atomizer has already been put into industrial operation.

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