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Microgravity combustion lecture 2

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D., 'Understanding Combustion Processes Through Microgravity Research,' Twenty ... Pergamon Press, 1993, pp. 49-66. Buckmaster, J., Zhang, Y. (1999) ... – PowerPoint PPT presentation

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Title: Microgravity combustion lecture 2


1
Microgravity combustion - lecture 2
  • Motivation
  • Time scales (Lecture 1)
  • Examples
  • Premixed-gas flames
  • Flammability limits (Lecture 1)
  • Stretched flames (Lecture 1)
  • Flame balls
  • Nonpremixed gas flames
  • Condensed-phase combustion
  • Particle-laden flames
  • Droplets
  • Flame spread over solid fuel beds
  • Reference Ronney, P. D., Understanding
    Combustion Processes Through Microgravity
    Research, Twenty-Seventh International Symposium
    on Combustion, Combustion Institute, Pittsburgh,
    1998, pp. 2485-2506

2
Nonpremixed-gas flames - counterflow
  • Counterflow flames
  • Nonpremixed flames less freedom of movement
    flame must lie where stoichiometric flux ratio
    maintained
  • Radiating gas volume flame thickness ?
  • Diffusion time scale ?2/? ?-1 ? ? (?/?)1/2
  • Computations µg experiments simple C-shaped
    dual-limit response
  • Conductive loss to burners at low ?? (?min)-1
    tcond d2/? (d burner spacing)
  • Need larger burners to see true radiation limit

CH4-N2 vs. air (Maruta et al. 1998)
3
Nonpremixed-gas flames - gas-jet flames
  • Roper (1977) Flame height (Lf) and residence
    time (tjet) determined by equating diffusion time
    (d2/D, d jet diameter, D oxygen diffusivity)
    to convection time (Lf/U)
  • Mass conservation U(0)d(0)2 U(Lf)d(Lf)2
    (round jet) U(0)d(0) U(Lf)d(Lf) (slot jet)
  • Buoyant flow U(Lf) (gLf)1/2 nonbuoyant
    U(Lf) U(0)
  • Consistent with more rigorous model based on
    boundary-layer theory (Haggard Cochran, 1972)

4
Gas-jet flames - results
  • Lf same at 1g or µg for round jet

Sunderland et al. (1999) - CH4/air
5
Flame widths at 1g and µg
  • tjet larger at µg than 1g for round jet
  • Larger µg flame width (Dtjet)1/2 - greater
    difference at low Re due to axial diffusion (not
    included in aforementioned models) buoyancy
    effects
  • Greater radiative loss fraction at µg ( 50 vs.
    8, Bahadori et al., 1993), thus cooler
    temperatures, redder color from soot

Sunderland et al. (1999) - CH4/air
6
Gas-jet flames - radiative loss
  • Estimate of radiative loss fraction (R)
    tjet/trad L/Utrad
  • R do2/Dtrad (momentum-controlled) (µg)
  • R (Udo2/gDtrad2)1/2 (buoyancy controlled)
    (low-speed 1g)
  • R(1g)/R(µg) (Re/Gr)1/2 for gases with D ? ?
    (Re Ud/? Gr gdo3/?2)
  • For typical do 1 cm, D 1 cm2/s (1 atm,
    T-averaged), R(1g)/R(µg) 1 at Re 1000
  • Lower Re R(1g)/R(µg) Re1/2 - much higher
    impact of radiative loss at µg

7
Flame lengths at 1g and µg
  • Low Re depends on Grashof or Froude number (Fr
    Re2/Gr)
  • 1g (low Fr) buoyancy dominated, teardrop shaped
  • µg (Fr 8) nearly diffusion-dominated, more
    like nonpremixed version of flame ball (similar
    to candle flame, fuel droplet flames discussed
    later)
  • High Re results independent of Fr

do 3.3 mm, Re 21 d 0.42 mm, Re
291 Sunderland et al. (1999) - C2H6/air
8
Turbulent flame lengths at 1g and µg
  • Turbulent flames (Hottel and Hawthorne, 1949)
  • D uLI u Uo LI do ? Lf do
    (independent of Re)
  • Bahadori et al. differences between 1g µg seen
    even at high Re - buoyancy effects depend on
    entire plume! (Cant get rid of buoyancy effects
    at high Re for turbulent flames!)

Hedge et al. (1997) - C3H8/air
9
Sooting gas-jet flames at 1g and µg
  • Reference Urban et al., 1998
  • Basic character of sooting flames same at 1g
    µg, but g affects temperature/time history (left)
    which in turn affects soot formation (right)

STS-94 space experiment (1997) Note soot emission
at high flow rate (beginning of test)
10
Sooting gas-jet flames at 1g and µg
11
Sooting gas-jet flames at 1g and µg
  • Typically greater at µg due to larger tjet -
    outweighs lower T
  • Smoke points seen at µg (Sunderland et al.,
    1994) - WHY???
  • tjet Uo1/2 for buoyant flames BUT...
  • tjet independent of Uo for nonbuoyant flames !
  • R (ideally) independent of U for nonbuoyant
    flames
  • Axial diffusion effects negligible at Re gt 50
  • Thermophoresis effects - concentrates soot in
    annulus

12
Particle-laden flames
  • This section courtesy of Prof. F. N. Egolfopoulos
  • Importance of particle-laden flows
  • Intentional/unintentional solid particle addition
  • Modification of ignition, burning, and extinction
    characteristics of gas phase
  • Propulsion (Al, B, Mg)
  • Power generation (coal)
  • Material synthesis
  • Explosions (lumber milling, grain elevators, mine
    galleries)
  • Particles are used in laser diagnostics (LDV,
    PIV, PDA)
  • Possible interactions between gas and particle
    phases
  • Dynamic (velocity modification)
  • Thermal (temperature modification)
  • Chemical (composition modification)
  • Parameters affecting these interactions
  • Physico-chemical properties of both phases
  • Fluid mechanics (strain rate)
  • Long range forces on particles (e.g. electric,
    magnetic, centrifugal, gravitational)
  • Phoretic forces on particles

13
Particle-laden flames - equations
  • Egolfopoulos and Campbell, 1999
  • Single particle momentum equation
  • Single particle energy equation

F ma
Stokes drag with correction for velocity slip at
high Kn
Thermophoretic force
Combined effects
Gravity force
14
Particle-laden flames in stagnation flows
  • Gravity effect on particle velocity (numerical)

Expected behavior
15
Particle-laden flames in stagnation flows
  • Gravity effect on particle velocity (numerical)

Note flow reversals
16
Particle-laden flames in stagnation flows
  • Gravity effect on particle number density and
    flux (numerical)

Results can NOT be readily derived from simple
arguments
17
Particle-laden flames in stagnation flows
  • Gravity effect on particle temperature
    (numerical)

Results NOT apparent
18
Premixed flame extinction by inert particles (1g
expts.)
  • Larger particles can more effectively cool down
    the flames - counter-intuitive result!

19
Premixed flame extinction (1g simulations)
  • Larger particles maintain larger temperature with
    the gas phase within the reaction zone!

Competition between surface and temperature
difference
20
Premixed flame extinction (1g simulations)
  • At high strain rates smaller particles cool more
    effectively
  • Reduced residence time for large particles
  • Surface effect becomes important

21
Premixed flame extinction (1g and µg expts.)
  • Extinction is facilitated at µg at 1g particles
    can not readily reach the top flame effect
    weaker for large particle loadings

22
Premixed flame extinction (1g µg simulations)
  • Low loading Particles do not reach upper flame
    in 1g
  • High loading Even at 1g particles penetrate the
    stagnation plane due to higher thermal expansion
    at higher ?

Low loading
High loading
23
Premixed flame extinction (1g µg expts)
  • Extinction if facilitated at µg argument about
    reduced particle velocities not applicable in
    this case!

Note Single flame extinction
24
Premixed flame extinction (1g µg simulations)
  • Extinction if facilitated at µg argument about
    reduced particle velocities not applicable in
    this case!
  • Gravity affects the particle number density
  • In µg particles possess more momentum and they
    are less responsive to thermal expansion that
    tends to decrease the particle number density ?
    more effective cooling

Note Single flame extinction
25
Premixed flame extinction (1g expts.)
  • Low strain rates reacting particles augment
    overall reactivity
  • High strain rates reacting particles act as
    inert cooling the gas phase and facilitating
    extinction

Note Single flame extinction
26
Summary - particle-laden flames
  • Direct effect on the trajectory of slow-moving
    particles
  • Indirect effects on particle
  • Number density
  • Temperature
  • Chemical activity
  • For inert particles, gravity has a noticeable
    effect on flame propagation and extinction
    through its modification of the particle dynamic
    and thermal states as well as on the particle
    number density
  • For reacting particles, gravity can render the
    solid phase inert thorugh its effect on the
    particle dynamic behavior

27
Droplet combustion
  • Spherically-symmetric model (Godsave, Spalding
    1953)
  • Steady burning possible - similar to flame balls
  • (large radii transport is diffusion-dominated)
  • Mass burning rate (p/4)?dddK K (8k/?dCP)
    ln(1B)
  • Flame diameter df dd ln(1B) / ln(1f)
  • Regressing droplet ddo2 - dd(t)2 Kt if
    quasi-steady
  • 1st µg experiment - Kumagai (1957) - K(µg) lt K(1g)

28
Droplet combustion
  • ... But large droplets NOT quasi-steady
  • K df/dd not constant - depend on ddo time
  • Large time scale for diffusion of radiative
    products to far-field O2 from far-field (like
    flame ball)
  • Soot accumulation dependent on ddo
  • Absorption of H2O from products by fuel
    (alcohols)

Marchese et al. (1999), heptane in O2-He
29
Droplets - extinction limits
  • Dual-limit behavior
  • Residence-time limited (small dd) tdrop df2/?
    tchem
  • Heat loss (large dd) (Chao et al., 1990) tdrop
    trad
  • Radiative limit at large dd confirmed by µg
    experiments
  • Extinction occurs at large dd, but dd decreases
    during burn - quasi-steady extinction not
    observable

Marchese, et al. (1999)
30
Droplets - extinction limits
  • Note flame never reaches quasi-steady diameter
  • df dd ln(1B)/ ln(1f) due to unsteadiness
    radiative loss effects
  • Extinguishment when flame diameter grows too
    large (closer to quasi-steady value)

Marchese, et al. (1999)
31
Droplets - radiation effects
  • Radiation in droplet flames can be a loss
    mechanism or can increase heat feedback to
    droplet (increased burning rate)
  • Problem of heat feedback severe with droplets -
    Stefan flow at surface limits conductive flux,
    causes ln(1B) term radiation not affected by
    flow
  • Add radiative flux (qr) to droplet surface
  • Crude estimates indicate important for practical
    flames, especially with exhaust-gas recirculation
    / reabsorption, but predictions never tested
    (PDRs proposals keep getting rejected)

32
Droplets - buoyancy effects
  • How important is buoyancy in droplet combustion?
  • Buoyant O2 transport / diffusive O2 transport
    effective diffusivity / DO2
  • Vbuoydf / DO2 0.3(gdf)1/2df/DO2
  • df 10dd, DO2 ? ? effective diffusivity /
    DO2 3.7Grd1/2 (Grd ? gdd3/?2)
  • ? K/Kg0 1 3.7Grd1/2
  • Experiment (Okajima Kumagai, 1982) K/Kg0 1
    0.53Grd.52 - scaling ok
  • Scaling Gr1/2 since df determined by
    stoichiometry, independent of V
  • If instead df ?/V then V (gdf)1/2
    (g?/V)1/2
  • ? V (g?)1/3, df (?2/g)1/3 ? Deff ? ? no
    change in K with Gr!
  • Moral need characteristic length scale that is
    independent of buoyancy to see increase in
    transport due to buoyancy

33
Soot formation in µg droplet combustion
  • Thermophoresis causes soot particles to migrate
    toward lower T (toward droplet), at some radius
    balances outward convection causes soot
    agglomeration shell to form

34
Candle flames
  • Similar to quasi-steady droplet but near-field
    not spherical
  • Space experiments (Dietrich et al., 1994, 1997)
  • Nearly hemispherical at µg
  • Steady for many minutes - probably gt df 2/?
  • Eventual extinguishment - probably due to O2
    depletion

1g µg
35
Candle flames - oscillations
  • Oscillations before extinguishment, except for
    small df
  • Near-limit oscillations of spherical flames?
    (Cheatham Matalon)
  • Edge-flame instability? (Buckmaster et al., 1999,
    2000)
  • Both models require high Le near-extinction
    conditions
  • Some evidence in droplets also (Nayagam et al.,
    1998)
  • Predicted but not seen in flame balls! (see
    STS-107 results)

36
References
  • M. G. Andac, F. N. Egolfopoulos, and C. S.
    Campbell, ''Premixed flame extinction by inert
    particles in normal- and micro-gravity,''
    Combustion and Flame 129, pp. 179-191, 2002.
  • M. G. Andac, F. N. Egolfopoulos, C. S. Campbell,
    and R. Lauvergne, ''Effects of inert dust clouds
    on the extinction of strained laminar flames,''
    Proc. Comb. Inst. 28, pp. 2921-2929, 2000.
  • Bahadori, M. Y., Stocker, D. P., Vaughan, D. F.,
    Zhou, L., Edelman, R. B., in Modern Developments
    in Energy Combustion and Spectroscopy, (F. A.
    Williams, A. K. Oppenheim, D. B. Olfe and M.
    Lapp, Eds.), Pergamon Press, 1993, pp. 49-66.
  • Buckmaster, J., Zhang, Y. (1999). Oscillating
    Edge Flames, Combustion Theory and Modelling 3,
    547-565.
  • Buckmaster, J., Hegap, A., Jackson, T. L. (2000).
    More results on oscillating edge flames.
    Physics of Fluids 12, 1592-1600.
  • Chao, B.H., Law, C.K., Tien, J.S., Twenty-Third
    Symposium (International) on Combustion,
    Combustion Institute, Pittsburgh, 1990, pp.
    523-531.
  • Cheatham, S., Matalon, M., Twenty-Sixth Symposium
    (International) on Combustion, Combustion
    Institute, Pittsburgh, 1996, pp. 1063-1070.
  • Egolfopoulos, F. N., Campbell, C. S. (1999).
    Dynamics and structure of dusty reacting flows
    Inert particles in strained, laminar, premixed
    flames, Combustion and Flame 117, 206-226.
  • Godsave G.A.E, Fourth Symposium (International)
    on Combustion, Williams and Wilkins, Baltimore,
    1953, pp. 818-830.
  • Haggard, J. B., Cochran, T. H., Combust. Sci.
    Tech. 5291-298 (1972).
  • Hegde, U., Yuan, Z. G., Stocker, D., Bahadori, M.
    Y., in Proceedings of the Fourth International
    Microgravity Combustion Workshop, NASA Conference
    Publication 10194, 1997, pp. 185-190.
  • Hottel, H. C., Hawthorne, W. R., Third Symposium
    (International) on Combustion, Combustion
    Institute, Pittsburgh, Williams and Wilkins,
    Baltimore, 1949, pp. 254-266.

37
References
  • Kumagai, S., Isoda, H., Sixth Symposium
    (International) on Combustion, Combustion
    Institute, Pittsburgh, 1957, pp. 726-731.
  • Okajim, S., Kumagai, S., Nineteenth Symposium
    (International) on Combustion, Combustion
    Institute, Pittsburgh, 1982, pp. 1021-1027.
  • S. L. Manzello, M. Y. Choi, A. Kazakov, F. L.
    Dryer, R. Dobashi, T. Hirano (2000). The
    burning of large n-heptance droplets in
    microgravity, Proceedings of the Combustion
    Institute 28, 10791086.
  • Marchese, A. J., Dryer, F. L., Nayagam, V.,
    Numerical Modeling of Isolated n-Alkane Droplet
    Flames Initial Comparisons With Ground and
    Space-Based Microgravity Experiments, Combust.
    Flame 116432459 (1999).
  • Maruta, K., Yoshida, M., Guo, H., Ju, Y., Niioka,
    T., Combust. Flame 112181-187 (1998).
  • Roper, F., Combust. Flame 29219-226 (1977).
  • Spalding, D.B., Fourth Symposium (International)
    on Combustion, Williams and Wilkins, Baltimore,
    1953, pp. 847-864.
  • Sunderland, P. B., Mendelson, B. J., Yuan, Z.-G.,
    Urban, D. L., Combust. Flame 116376-386 (1999).
  • Urban, D. L, et al., Structure and soot
    properties of nonbuoyant ethylene/air laminar jet
    diffusion flames, AIAA Journal, Vol. 36, pp.
    1346-1360 (1998).
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