2017
DOI: 10.1016/j.combustflame.2017.02.035
|View full text |Cite
|
Sign up to set email alerts
|

Fuel effects on lean blow-out in a realistic gas turbine combustor

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
2
1
1
1

Citation Types

0
27
0
1

Year Published

2017
2017
2024
2024

Publication Types

Select...
4
4

Relationship

1
7

Authors

Journals

citations
Cited by 160 publications
(39 citation statements)
references
References 42 publications
0
27
0
1
Order By: Relevance
“…The inner tube of the fuel stream is recessed from the jet exit plane by L r = 75 mm, with the bulk jet velocity is set to 57 m/s (Lr75-57 ), corresponding to 50% of the experimentally measured blow-off velocity. The recess results in a partially premixed reactant-gas mixture, which is relevant to modern gas turbine applications [46,47].…”
Section: Methodsmentioning
confidence: 99%
“…The inner tube of the fuel stream is recessed from the jet exit plane by L r = 75 mm, with the bulk jet velocity is set to 57 m/s (Lr75-57 ), corresponding to 50% of the experimentally measured blow-off velocity. The recess results in a partially premixed reactant-gas mixture, which is relevant to modern gas turbine applications [46,47].…”
Section: Methodsmentioning
confidence: 99%
“…In particular, the methane content in the fuel gas composition has a decisive influence on the energy characteristics of the gas turbine and on the performance of the installation as a whole. [13][14][15].…”
Section: Discussionmentioning
confidence: 99%
“…The prediction of such phenomena, that imply transients of the local flame structure, is one of the main challenges of current generation turbulent combustion models since the interaction between turbulence and chemistry has to be accurately captured to have reliable predictions. Although some success in predicting local extinctions has been shown with flamelet-based models [84,85], methods based on the online solution of the chemistry appear the most appropriate since it is possible to directly take into account the interaction between turbulence and flame structure, with the former directly affecting the transient evolution of the species. Furthermore, the presence of liquid sprays, as in typical gas turbines for aeronautical application, further increases the range of scales and physical processes involved in the combustion process [34] generally making the prediction of the flame behavior more challenging.…”
Section: Turbulent Combustion Modelsmentioning
confidence: 99%
“…At the same time, the flame moves closer to the injection location with evaporation strongly affecting also the local extinction behaviour. Recently, complete blow-off of a spray combustor has also been attempted with the progress variable-flamelet model [84] and reasonable prediction of the structure of the flame at the blow-off condition was made. In addition, the "Lean Blow-Out" (LBO, as global extinction is known in gas turbine combustion parlance) was simulated and the important role of evaporation in determining the [124,133].…”
Section: Examplesmentioning
confidence: 99%
See 1 more Smart Citation