1974
DOI: 10.1016/0094-5765(74)90028-9
|View full text |Cite
|
Sign up to set email alerts
|

Combustion of droplets in sprays

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
2
2

Citation Types

0
13
0

Year Published

1980
1980
2017
2017

Publication Types

Select...
8
1

Relationship

0
9

Authors

Journals

citations
Cited by 82 publications
(15 citation statements)
references
References 6 publications
0
13
0
Order By: Relevance
“…The maximum flamelet temperature was 2000°C close to the burner but dropped drastically above 0.6 cm to approximately 500°C at 4 cm by mixing with the surrounding gas. 25 In contrast, the maximum spray flame temperature was 2300°C up to a height of 5 cm. Droplets containing solvent and precursor continuously evaporate and supply FIG.…”
Section: A Spray Flame Characterizationmentioning
confidence: 99%
See 1 more Smart Citation
“…The maximum flamelet temperature was 2000°C close to the burner but dropped drastically above 0.6 cm to approximately 500°C at 4 cm by mixing with the surrounding gas. 25 In contrast, the maximum spray flame temperature was 2300°C up to a height of 5 cm. Droplets containing solvent and precursor continuously evaporate and supply FIG.…”
Section: A Spray Flame Characterizationmentioning
confidence: 99%
“…This evaporation region is observed also in classic fuel spray combustion. 25 It is attributed to fuel mass transfer limitation that slows the combustion and prolongs the high temperature region. The distinctive constant temperature region can be shortened, for example, by increasing the oxidant flow.…”
Section: A Spray Flame Characterizationmentioning
confidence: 99%
“…With the increase in pressure, the exit flow velocity of the tangential swirl air is increased, which increases the angular momentum and the swirl intensity. 26 Burning SRF particles can be seen as small specks of light on the darker background, and have also been highlighted by blue circles.…”
mentioning
confidence: 99%
“…11 When the liquid fuel is injected from the center of the jet into its periphery, as is the case discussed in the present paper, a signi cant reduction of the droplet size and the drag on the fuel droplets injected along the center is, therefore, expected, and this will reduce the penetration of the droplets into the external jet shear layer. The experiments in this paper support this expectation, as will be shown later.…”
Section: Introductionmentioning
confidence: 93%