Combustion Turbulence Flow in the Advanced Vortex Combustor with Built-In Obstacles
To obtain the advanced vortex combustor (AVC) and its optimal structure parameters in light of built-in obstacles, numerical simulation was performed. This research shows that inclined struts have optimal structural parameters with inclination angle α=30° and blocking ratio BR=12%, while guide vane...
Saved in:
Main Authors: | Yu Chen, Zhuoxiong Zeng, Haoyuan Wang |
---|---|
Format: | Article |
Language: | English |
Published: |
Wiley
2021-01-01
|
Series: | International Journal of Aerospace Engineering |
Online Access: | http://dx.doi.org/10.1155/2021/7410747 |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Similar Items
-
Numerical Analysis of Turbulent Combustion in a Model Swirl Gas Turbine Combustor
by: Ali Cemal Benim, et al.
Published: (2016-01-01) -
Experimental and Computational Study of Trapped Vortex Combustor Sector Rig with High-Speed Diffuser Flow
by: R. C. Hendricks, et al.
Published: (2001-01-01) -
Numerical Simulation of Combustion and Rotor-Stator Interaction in a Turbine Combustor
by: Dragos D. Isvoranu, et al.
Published: (2003-01-01) -
Numerical Simulation of Combustion and Rotor-Stator Interaction in a Turbine Combustor
by: Isvoranu D. a., et al.
Published: (2003-01-01) -
Combustion Characteristics of Mui and Taru Basin Coal in a Fluidized Bed Combustor
by: Brian Ondari, et al.
Published: (2021-01-01)