Nw. Chang et al., Spatially resolved flamelet statistics for reaction rate modeling using premixed methane-air flames in a near-homogeneous turbulence, COMB FLAME, 127(1-2), 2001, pp. 1880-1894
Flamelet models have been widely applied to predict premixed turbulent comb
ustion, such as for instance, the Bray-Moss-Libby (BML) model in which spat
ial flamelet statistics and, thus, mean reaction rate were deduced from a m
ean reaction progress variable ((c) over bar) and a mean crossing frequency
. Recently, Shy et al. introduced a methodology based upon a downward propa
gating premixed flame through a near-isotropic turbulent flow field in a cr
uciform burner with a pair of specially designed ion probes for quantitativ
e measurements of turbulent burning velocities. In this work, we report det
ailed measurements of important spatial statistical properties of these pro
pagating turbulent methane-air flames for experimental analysis of the BML
model using high-speed laser sheet tomography technique. Four cases are stu
died, including both lean and rich conditions, with equivalence ratio phi =
0.9 and 1.2, and two different turbulent intensities n'/S-L approximate to
1.4 and 4.1 where S-L is the laminar burning velocity. Each case contains
up to five hundred runs at the same experimental conditions, so that suffic
ient images in the central near-isotropic region can be obtained to extract
contours of reaction progress variable ((c) over cap), flamelet crossing l
engths, crossing frequencies, flame wrinkling lengths ((L) over cap (y)), f
lamelet crossing angles (theta), coefficient g in the BML model, and flame
surface density (Sigma).
The symmetric profile of flamelet crossing frequency v(y) as a function of
(c) over bar is found for diffusionally stable flames, where the maximum va
lue of v(y) occurs at (c) over bar = 0.5. For diffusionally unstable flames
, the profile of v(y) tends to be asymmetric (skewed to the burned side), r
evealing the effect of Lewis number on vy. It is found that v(y), evaluated
along contours of (c) over bar, is almost constant for all values of (c) o
ver bar. Its magnitude decreases with increasing turbulent intensities and
is much smaller than the integral length scale in the unreacted turbulent f
low. As Lewis number is varied, values of (L) over cap (y) for diffusionall
y unstable flames are larger than that for diffusionally stable flame. Thes
e results differ from those obtained with Bunsen flames and liquid flames,
indicating that the BML model needs a precise closure for (L) over cap (y).
The overall mean cosine value of theta (= sigma (y)) is measured to be 0.6
1 for u'/S-L approximate to 1.4 and 0.67 for u'/S-L approximate to 4.1, in
contrast to 0.5 found for Bunsen flames but very close to 0.65 measured in
liquid flames, suggesting that sigma (y) is probably not a universal consta
nt its assumed by the BML model. The coefficient g is found to be better de
scribed by an exponential relationship (g = 2) than a gamma-two relationshi
p (g = 1), a result consistent with previous Bunsen flame measurements. Oth
er quantities of interest, such as crossing frequencies, auto-correlations
of c, and distributions of actual crossing angle along (c) over bar contour
s, are also examined. These results may be used to improve the BML model. (
C) 2001 by The Combustion Institute.