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Second-moment computation of strongly-swirling reacting flow in a model combustor

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Numerical Combustion

Part of the book series: Lecture Notes in Physics ((LNP,volume 351))

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Abstract

The paper reports a computational effort directed towards the modelling of a turbulent, swirling and reacting propane-air flow in a laboratory combustor. The study focuses, in particular, on the performance of a Favre-averaged second-moment closure, applied in conjunction with an equilibrium-combustion model and the so-called β-probability density function. The above model is applied within the framework of a finite-volume scheme incorporating a quadratic approximation for convection. Some results are presented for non-reacting conditions, but the majority of comparisons relate to the reacting case. These comparisons demonstrate that, in contrast to previous experience with non-reacting flows, no decisive advantages are gained from second-moment modelling in the particular case examined, and this is attributed to the dominance of combustion-model defects.

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Abbreviations

Ap:

Finite-volume coefficient related node at cell centre

a, b:

Constants in β-p.d.f.

C:

Density-weighted mean scalar

Cc,CD,Ck :

Constants in second-moment

Cε, Cε1 :

closure

Cε2,Cε3, Cμ D:

Combustor diameter

f:

Fuel mixture fraction

Gij/Gi,c :

Additional stress/flux generation terms in density-weighted closure

k:

Turbulence kinetic energy

m:

Iteration level

n:

Time level

P:

Pressure

P(f):

Probability density function

Pij/Pi,c :

Stress/flux generation terms

Rij/Ri,c :

Additive stress/flux contributions arising from axial symmetry and swirl

r:

Radial coordinate

Sij :

Source term in finite-volume equation

U:

Axial velocity component

Ũi :

Density-weighted mean velocity in tensor direction i

≈:

Density-weighted scalar-flux

ui"uj":

Density-weighted Reynolds-stress

V:

Radial velocity component

Vol:

Volume of finite-volume cell

W:

Swirl velocity component

x:

Axial coordinate

xi :

Coordinate in tensor direction i

αct :

Relaxation parameters

δij :

Kronecker delta

Δr :

Radial height of control-volume

Δt :

Time step

Δx:

Axial length of control-volume

ɛ:

Turbulence energy dissipation rate

ζ:

Constant in equations (7)

μapp :

Pseudo-viscosity

ϱ:

Density

ϕ:

General flow variable

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Alain Dervieux Bernard Larrouturou

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© 1989 Springer-Verlag

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Hogg, S., Leschziner, M.A. (1989). Second-moment computation of strongly-swirling reacting flow in a model combustor. In: Dervieux, A., Larrouturou, B. (eds) Numerical Combustion. Lecture Notes in Physics, vol 351. Springer, Berlin, Heidelberg. https://doi.org/10.1007/3-540-51968-8_96

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  • DOI: https://doi.org/10.1007/3-540-51968-8_96

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  • Publisher Name: Springer, Berlin, Heidelberg

  • Print ISBN: 978-3-540-51968-3

  • Online ISBN: 978-3-540-46866-0

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