Flame stabilization at moderate flow swirling

Author(s):  
Oleg V. Matvienko ◽  
Alena E. Litvinova
1997 ◽  
Author(s):  
E. Koc-Alkislar ◽  
L. Lourenco ◽  
A. Krothapalli ◽  
P. Strykowski ◽  
E. Koc-Alkislar ◽  
...  

Author(s):  
A. Yu. Krainov ◽  
◽  
K. M. Moiseeva ◽  
V. A. Poryazov ◽  
◽  
...  

A numerical study of combustion of the aluminum-air suspension in the swirling flow in the expansion chamber has been performed. The physical and mathematical formulation of the problem is based on the dynamic model of the multiphase reacting media.


1994 ◽  
Vol 99 (2) ◽  
pp. 288-294 ◽  
Author(s):  
Jing-Tang Yang ◽  
Chang-Wu Yen ◽  
Go-Long Tsai

Author(s):  
J.P. Longwell ◽  
J.E. Chenevey ◽  
W.W. Clark ◽  
E.E. Frost

2019 ◽  
Vol 18 ◽  
pp. 104-108
Author(s):  
Lakka Suneetha ◽  
P. Randive ◽  
K.M. Pandey

2012 ◽  
Vol 26 (7) ◽  
pp. 4284-4290 ◽  
Author(s):  
Dae Hoon Lee ◽  
Kwan-Tae Kim ◽  
Hee Seok Kang ◽  
Young-Hoon Song ◽  
Jae Eon Park

AIAA Journal ◽  
1964 ◽  
Vol 2 (11) ◽  
pp. 2030-2031
Author(s):  
JAMES R. MAUS ◽  
WILLIAM T. SNYDER

1981 ◽  
Vol 103 (1) ◽  
pp. 34-42 ◽  
Author(s):  
J. R. Shekleton

The Radial Engine Division of Solar Turbines International, an Operating Group of International Harvester, under contract to the U.S. Army Mobility Equipment Research & Development Command, developed and qualified a 10 kW gas turbine generator set. The very small size of the gas turbine created problems and, in the combustor, novel solutions were necessary. Differing types of fuel injectors, combustion chambers, and flame stabilizing methods were investigated. The arrangement chosen had a rotating cup fuel injector, in a can combustor, with conventional swirl flame stabilization but was devoid of the usual jet stirred recirculation. The use of centrifugal force to control combustion conferred substantial benefit (Rayleigh Instability Criteria). Three types of combustion processes were identified: stratified and unstratified charge (diffusion flames) and pre-mix. Emphasis is placed on five nondimensional groups (Richardson, Bagnold, Damko¨hler, Mach, and Reynolds numbers) for the better control of these combustion processes.


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