DocumentCode :
2448926
Title :
Numerical investigation in cold flow field on the influence of the injection velocity from the center body of the trapped vortex combustor
Author :
Liu, Shiqing ; Zhong, Jingjun
Author_Institution :
Marine Eng. Coll., Dalian Maritime Univ., Dalian, China
fYear :
2011
fDate :
24-26 June 2011
Firstpage :
2279
Lastpage :
2283
Abstract :
The trapped vortex combustor is attracted attention on its performance of low flow resistance, strong combust stability and low oil limity. The numerical investigation has been taken on the field in and out of the trapped vortex cavity of the trapped vortex combustor in cold flow field with different velocity of the nozzle located on the forbody and afterbody. The result shows that the stability of the trapped vortex is conformed and the trapped vortex becomes uniform. The total press loss on the outlet of the combustor is increased with the speed of the injection gets bigger. The press in the trapped vortex cavity is increased too. The mass average velocity in the trapped vortex cavity becomes higher when the injection speed crease on the forebody, the turbulence increase too. But when the injection speed on the after body increases, the mass average velocity in the trapped vortex cavity becomes low and the becomes high, the turbulence becomes low.
Keywords :
combustion equipment; nozzles; turbulence; vortices; cold flow field; combustion stability; injection speed; injection velocity; mass average velocity; nozzle; trapped vortex cavity; trapped vortex combustor; turbulence; Cavity resonators; Combustion; Educational institutions; Industries; Numerical stability; Presses; Stability analysis; Cold Flow Field; Injection Speed; Numerical Investigation; Trapped Vortex Combusto;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Remote Sensing, Environment and Transportation Engineering (RSETE), 2011 International Conference on
Conference_Location :
Nanjing
Print_ISBN :
978-1-4244-9172-8
Type :
conf
DOI :
10.1109/RSETE.2011.5964765
Filename :
5964765
Link To Document :
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