Abstract
Ignition and combustion of a condensed fuel in a gaseous high temperature oxidizing boundary layer flow is analyzed on the basis of higher order boundary layer theory. First order effects due to displacement thickness are taken into account and the pressure gradients generated in the outer potential flow are included in the numerical solution of the governing equations. The strong positive pressure gradients which are induced by expansion in front of the flame generate a low velocity region which facilitates a longitudinal diffusion of heat and mass.
Zusammenfassung
Es wird die Zündung und Verbrennung eines festen Brennstoffs in einer heißen gasförmigen oxidierenden Grenzschichtströmung auf der Grundlage der Grenzschichttheorie höherer Ordnung untersucht. Effekte erster Ordnung aufgrund der Verdrängungsdicke werden berücksichtigt und Druckgradienten, die in der äußeren Potentialströmung erzeugt werden, sind in der numerischen Lösung der Bestimmungsgleichungen eingeschlossen. Die starken positiven Druckgradienten, die durch die Expansion vor der Flamme induziert werden, erzeugen ein Gebiet niedriger Geschwindigkeit, was einen Wärme- und Stofftransport entgegen der Hauptströmungsrichtung ermöglicht.
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Abbreviations
- A :
-
preexponential factor for the gas-phase chemical reaction
- D *± :
-
diffusion coefficient of speciesα
- Ec :
-
Eckert number defined in Eq. (12)
- f :
-
non-dimensional stream function introduced in Eq. (34)
- L :
-
non-dimensional latent heat of vaporization defined in Eq. (42)
- L *c :
-
characteristic length given in Eq. (40)
- P :
-
non-dimensional pressure defined in Eq. (7)
- Pr :
-
Prandtl number Pr=μ *∞ c *p /λ*
- Q :
-
non-dimensional heat release defined in Eq. (23)
- R :
-
Reynolds number R=ϱ *∞ u *∞ L *c /μ *∞
- S :
-
non-dimensional coordinate defined in Eq. (23)
- Scα :
-
Schmidt number for speciesα Scα=μ *∞ /ϱ*D *α
- T *a :
-
activation temperature of the gas-phase chemical reaction
- T*:
-
temperature
- u *i :
-
cartesian components of the fluid velocity
- V :
-
non-dimensional transversal fluid velocity
- ωα :
-
generation rate of speciesα in mol per unit time unit volume
- Wa :
-
molecular weight of speciesα
- x*:
-
longitudinal coordinate
- x *i :
-
cartesian coordinates
- Yα :
-
mass concentration of speciesα
- yα :
-
reduced mass concentration of speciesα defined in Eq. (35)
- δ ij :
-
Kronecker delta; 0 fori ≠j, 1 fori =j
- η :
-
non-dimensional similarity coordinate defined in Eq. (34)
- λ*:
-
coefficient of thermal conduction
- μ*:
-
coefficient of viscosity
- vα :
-
stoichiometric coefficient of speciesα
- ρ*:
-
gas density
- ø :
-
non-dimensional temperature defined in Eq. (35)
- Φ :
-
dissipation function
- φ :
-
stream function defined in Eq. (30)
- ∞ :
-
free stream
- α :
-
refers to species
- ∼:
-
outer flow
- *:
-
dimensional variable
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Treviño, C., Stüttgen, W. & Peters, N. Pressure gradients due to gas expansion in the boundary layer combustion of a condensed fuel. Wärme- und Stoffübertragung 25, 309–319 (1990). https://doi.org/10.1007/BF01780744
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DOI: https://doi.org/10.1007/BF01780744