DocumentCode
1680543
Title
Study on the Symmetry of Shuttle-type Cavity in Supersonic Flow
Author
Wu, Jinxiang ; Ma, Jing
Author_Institution
Sch. of Energy & Environ. Eng., Hebei Univ. of Technol., Tianjin, China
fYear
2012
Firstpage
675
Lastpage
678
Abstract
The supersonic combustion chamber with Shuttle-type cavity was investigated numerically and experimentally. The symmetry of Shuttle-type cavity is discussed in this paper. Results show that the symmetry is determined by the number of low-pressure centre area. Mach number of main flow is the key factor that determines the symmetrical characteristic of Shuttle-type cavity flow field and the critical Mach number is 1.6 in our calculation condition.
Keywords
Mach number; cavitation; supersonic flow; Mach number; shuttle-type cavity flow field; supersonic combustion chamber; supersonic flow; symmetrical characteristic; Cavity resonators; Combustion; Fluids; Fuels; Mathematical model; Numerical models; Surface treatment; Shuttle-type cavity; supersonic flow; symmetry;
fLanguage
English
Publisher
ieee
Conference_Titel
Computer Distributed Control and Intelligent Environmental Monitoring (CDCIEM), 2012 International Conference on
Conference_Location
Hunan
Print_ISBN
978-1-4673-0458-0
Type
conf
DOI
10.1109/CDCIEM.2012.165
Filename
6178592
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