1998
DOI: 10.2514/3.13970
|View full text |Cite
|
Sign up to set email alerts
|

Method for generating equilibrium swirling inflow conditions

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
2
1
1
1

Citation Types

0
45
0

Year Published

2003
2003
2020
2020

Publication Types

Select...
7
1

Relationship

1
7

Authors

Journals

citations
Cited by 30 publications
(45 citation statements)
references
References 0 publications
0
45
0
Order By: Relevance
“…1. Just as the reverseflow cyclone, it has a tangential inlet which can be directly incorporated in the simulation procedure, thereby avoiding the need to separately generate swirl-inflow conditions, such as done by Pierce and Moin [12] in the context of their LES. In contrast to the reverse flow generated in the cyclone, the vortex tube facility generates a unidirectional flow.…”
Section: Introductionmentioning
confidence: 99%
“…1. Just as the reverseflow cyclone, it has a tangential inlet which can be directly incorporated in the simulation procedure, thereby avoiding the need to separately generate swirl-inflow conditions, such as done by Pierce and Moin [12] in the context of their LES. In contrast to the reverse flow generated in the cyclone, the vortex tube facility generates a unidirectional flow.…”
Section: Introductionmentioning
confidence: 99%
“…The founder idea of large eddy simulation (LES) is to resolve the large turbulent motions in a flow field and to modeling only the effects of small ones. The resolved contribution ̅ is obtained by applying the spatial LES filter to instantaneous variables f. Filtering the instantaneous governing equations and introducing the Favre filtered variables /   ff [17][18].…”
Section: Mathematical Formulationmentioning
confidence: 99%
“…Once the CTRZ is established, it anchors the flame, thus improving the flame stabilization by returning hot gases and active radicals back to the jet core leading to a more stirred mixture. The shear layer between this recirculation zone and the main flow zone also generates great amount of turbulent energy, which intensifies the air-fuel mixing process and therefore improves the combustion efficiency, reduces the flame length, and lowers significantly the emission of NOx [14][15][16][17][18][19].…”
Section: Introductionmentioning
confidence: 99%
“…In both cases of N29S054 and N16S159, the top-hat profile at the inflow boundary remains to exist in a smaller extent in the numerical re-sults. In order to address this kind of difficulty in specifying the boundary condition at the inflow, Pierce and Moin (9), (10) used the LES of the flow in the coaxial annular duct to generate the swirl inflow condition, and analyzed the combustor with swirler. In these problem setup, however, the flow field which stipulates the inflow boundary condition is not independent of the combustion flow field with swirl under discussion, and they are mutually and simultaneously dependent, so this technique is not a perfect solution.…”
Section: Velocity Fieldmentioning
confidence: 99%