2016
DOI: 10.1016/j.combustflame.2016.01.004
|View full text |Cite
|
Sign up to set email alerts
|

Effect of pressure on hydrogen/oxygen coupled flame–wall interaction

Abstract: The design and optimization of liquid-fuel rocket engines is a major scientific and technological challenge. One particularly critical issue is the heating of solid parts that are subjected to extremely high heat fluxes when exposed to the flame. This in turn changes the injector lip temperature, leading to possibly different flame behaviors and a fully coupled system. As the chamber pressure is usually much larger than the critical pressure of the mixture, supercritical flow behaviors add even more complexity… Show more

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
4
1

Citation Types

0
11
0

Year Published

2017
2017
2024
2024

Publication Types

Select...
6
2
1

Relationship

0
9

Authors

Journals

citations
Cited by 20 publications
(11 citation statements)
references
References 31 publications
(63 reference statements)
0
11
0
Order By: Relevance
“…However, since the temperature variations in combustion systems are of several hundreds Kelvins or even a couple of thousands Kelvins, the absolute level of wall temperature variations is not necessarily negligible. This is even significant in extreme conditions as met in high-pressure hydrogen/oxygen flames whose transient flame-wall interaction has recently been studied numerically with transient CHT simulations of 1D head-on quenching [7].…”
Section: Contextmentioning
confidence: 99%
“…However, since the temperature variations in combustion systems are of several hundreds Kelvins or even a couple of thousands Kelvins, the absolute level of wall temperature variations is not necessarily negligible. This is even significant in extreme conditions as met in high-pressure hydrogen/oxygen flames whose transient flame-wall interaction has recently been studied numerically with transient CHT simulations of 1D head-on quenching [7].…”
Section: Contextmentioning
confidence: 99%
“…While subgrid-scale modeling efforts are still ongoing, the range of applications of such high-fidelity computations widens to new horizons such as multiphysics simulations of conjugate heat transfer (CHT). Several applications to turbine blades have been reported [9,10] as well as combustion cases [22,2,31]. The accurate prediction of heat flux and temperature at the combustor wall requires accounting for the coupling between the turbulent reactive flow, the heat conduction within the walls and the radiative energy transfer.…”
Section: Introductionmentioning
confidence: 99%
“…Using a detailed approach such as large-eddy simulation (LES) in a multiphysics framework is a promising candidate to accurately predict the wall temperature field. Such a combination of LES and conjugate heat transfer (CHT) has already been applied to several combustion applications [18][19][20]. When radiative energy transfer must be accounted for, the LES code is coupled to a solver of the radiative transfer equation [21][22][23].…”
Section: Introductionmentioning
confidence: 99%