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AME 513 Principles of Combustion Lecture 10 Premixed flames III: Turbulence effects
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2 AME 514 - Fall 2012 - Lecture 10 - Premixed flames III Motivation Study of premixed turbulent combustion important because Turbulence increases mean flame propagation rate (S T ) and thus mass burning rate (= S T A projected ) If this trend increased ad infinitum, arbitrarily lean mixtures (low S L ) could be burned arbitrarily fast by using sufficiently high u’...but too high u' leads to extinction - nixes that idea Even without forced turbulence, if the Grashof number gd 3 / 2 is larger than about 10 6 (g = 10 3 cm/s 2, ≈ 1 cm 2 /s d > 10 cm), turbulent flow will exist due to buoyancy Examples Premixed turbulent flames »Gasoline-type (spark ignition, premixed-charge) internal combustion engines »Stationary gas turbines (used for power generation, not propulsion) Nonpremixed flames »Diesel-type (compression ignition, nonpremixed-charge) internal combustion engines »Gas turbines »Most industrial boilers and furnaces
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3 AME 514 - Fall 2012 - Lecture 10 - Premixed flames III Turbulent burning velocity Models of premixed turbulent combustion don’t agree with experiments nor each other!
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4 AME 514 - Fall 2012 - Lecture 10 - Premixed flames III Basics of turbulence Good reference: Tennekes: “A First Course in Turbulence” Job 1: need a measure of the strength of turbulence Define turbulence intensity (u’) as rms fluctuation of instantaneous velocity u(t) about mean velocity ( )
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5 AME 514 - Fall 2012 - Lecture 10 - Premixed flames III Basics of turbulence Job 2: need a measure of the length scale of turbulence Define integral length scale (L I ) as A measure of size of largest eddies Largest scale over which velocities are correlated Typically related to size of system (tube or jet diameter, grid spacing, …) Here the overbars denote spatial (not temporal) averages A(r) is the autocorrelation function at some time t Note A(0) = 1 (fluctuations around the mean are perfectly correlated at a point) Note A(∞) = 0 (fluctuations around the mean are perfectly uncorrelated if the two points are very distant) For truly random process, A(r) is an exponentially decaying function A(r) = exp(-r/L I )
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6 AME 514 - Fall 2012 - Lecture 10 - Premixed flames III Basics of turbulence In real experiments, generally know u(t) not u(x) - can define time autocorrelation function A(x, ) and integral time scale I at a point x Here the overbars denote temporal (not spatial) averages With suitable assumptions L I = (8/π) 1/2 u’ I Define integral scale Reynolds number Re L u’L I / (recall = kinematic viscosity) Note generally Re L ≠ Re flow = Ud/ ; typically u’ ≈ 0.1U, L I ≈ 0.5d, thus Re L ≈ 0.05 Re flow Turbulent viscosity T Molecular gas dynamics: ~ (velocity of particles)(length particles travel before changing direction) By analogy T ~ u’L I or T / = C Re L ; C ≈ 0.061 Similarly, turbulent thermal diffusivity T / ≈ 0.042 Re L
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7 AME 514 - Fall 2012 - Lecture 10 - Premixed flames III Turbulent burning velocity Experimental results shown in Bradley et al. (1992) smoothed data from many sources, e.g. fan-stirred bomb
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8 AME 514 - Fall 2012 - Lecture 10 - Premixed flames III = S T /S L Bradley et al. (1992) Compilation of data from many sources = u’/S L
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9 AME 514 - Fall 2012 - Lecture 10 - Premixed flames III Characteristics of turbulent flames Most important property: turbulent flame speed (S T ) Most models based on physical models of Damköhler (1940) Behavior depends on Karlovitz number (Ka) Low Ka: “Huygens propagation,” thin fronts that are wrinkled by turbulence but internal structure is unchanged High Ka: Distributed reaction zones, broad fronts Defined using cold- gas viscosity
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10 AME 514 - Fall 2012 - Lecture 10 - Premixed flames III Characteristics of turbulent flames
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11 AME 514 - Fall 2012 - Lecture 10 - Premixed flames III Turbulent combustion regimes Comparison of flamelet and distributed combustion (Yoshida, 1988) Flamelet: temperature is either T ∞ or T ad, never between, and probability of product increases through the flame Distributed: significant probability of temperatures between T ∞ or T ad, probability of intermediate T peaks in middle of flame
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12 AME 514 - Fall 2012 - Lecture 10 - Premixed flames III Estimates of S T in flamelet regime Damköhler (1940): in Huygens propagation regime, flame front is wrinkled by turbulence but internal structure and S L are unchanged Propagation rate S T due only to area increase via wrinkling: S T /S L = A T /A L S T /S L = A T /A L
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13 AME 514 - Fall 2012 - Lecture 10 - Premixed flames III Estimates of S T in flamelet regime Low u’/S L : weakly wrinkled flames S T /S L = 1 + (u’/S L ) 2 (Clavin & Williams, 1979) - standard for many years Actually Kerstein and Ashurst (1994) showed this is valid only for periodic flows - for random flows S T /S L - 1 ~ (u’/S L ) 4/3 Higher u’/S L : strongly wrinkled flames Schelkin (1947) - A T /A L estimated from ratio of cone surface area to base area; height of cone ~ u’/S L ; result Other models based on fractals, probability-density functions, etc., but mostly predict S T /S L ~ u’/S L at high u’/S L with the possibility of “bending” or quenching at sufficiently high Ka ~ (u’/S L ) 2, e.g. Yakhot (1988):
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14 AME 514 - Fall 2012 - Lecture 10 - Premixed flames III Effects of thermal expansion Byckov (2000): Same as Yakhot (1988) if no thermal expansion ( = 1) Also says for any , if u’/S L = 0 then S T /S L = 1; probably not true
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15 AME 514 - Fall 2012 - Lecture 10 - Premixed flames III S T in distributed combustion regime Much less studied than flamelet combustion Damköhler (1940): A ≈ 0.25 (gas); A ≈ 6.5 (liquid) Assumption T ≈ L probably not valid for high ; recall …but probably ok for small Example: 2 equal volumes of combustible gas with E = 40 kcal/mole, 1 volume at 1900K, another at 2100K (1900) ~ exp(-40000/(1.987*1900)) = 3.73 x 10 4 (2100) ~ exp(-40000/(1.987*2100)) = 1.34 x 10 4 Average = 2.55 x 10 4, whereas (2000) = 2.2 x 10 4 (16% difference)! Averaging over ±5% T range gives 16% error!
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