2002
DOI: 10.1016/s0010-2180(02)00368-1
|View full text |Cite
|
Sign up to set email alerts
|

Markstein numbers in counterflow, methane- and propane- air flames: a computational study

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
2
1
1
1

Citation Types

5
70
0
1

Year Published

2010
2010
2020
2020

Publication Types

Select...
7

Relationship

0
7

Authors

Journals

citations
Cited by 91 publications
(76 citation statements)
references
References 36 publications
5
70
0
1
Order By: Relevance
“…However, this does not pose a problem here because only the velocity of the cold gas ahead of the flame appears in the theory leading to Eqs. 1 and 2; see [1][2][3][4][5]. Comparisons with flames in unseeded mixtures show that the additional fuel in the oil drops has no noticeable effect on the flame.…”
Section: Experimental Setup and Techniquesmentioning
confidence: 99%
See 2 more Smart Citations
“…However, this does not pose a problem here because only the velocity of the cold gas ahead of the flame appears in the theory leading to Eqs. 1 and 2; see [1][2][3][4][5]. Comparisons with flames in unseeded mixtures show that the additional fuel in the oil drops has no noticeable effect on the flame.…”
Section: Experimental Setup and Techniquesmentioning
confidence: 99%
“…However, the question arises as to what extent can these results be used for real flames of finite thickness, for which even the definitions of propagation velocity and front curvature are ambiguous. For planar stationary flames in the stagnation point flow, the question has been addressed by Davis et al [4,5], who used numerical computations to show that Eqs. 1 and 2 can still be used if the velocity U n and the strain rate are understood as those of the cold gas upstream of the flame (the outer solution in the asymptotic description) extrapolated to the reaction region of the flame.…”
Section: Introductionmentioning
confidence: 99%
See 1 more Smart Citation
“…The subscripts u and b refer respectively to unburnt and burnt gases. Using the values of Ma determined by Davis et al [33] and following the same approach as in [28], three characteristic lengths can be calculated:…”
Section: : Discussionmentioning
confidence: 99%
“…To understand the flame dynamics and flame structure clearly, some researchers (Davis et al [43], Akkerman and Bychkov [44], et al) have provided detailed data and results on the inner mechanism of laminar flame structure change, such as the laminar flame velocity, the effective flame thickness, the ratio of the unburnt to burnt gas density and the effective Markstein number. The relevant dynamic parameters in Table 1 can be used as a reference to describe the flame dynamics and flame structure [42].…”
Section: Flame Structure Characteristic Based On High Speed Schlierenmentioning
confidence: 99%