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NCSU MAE

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Because the radial flame position was not noted with the height, ... For flames stabilized at h 10d, the normalized fluctuations. are generally above 0.3h. ... – PowerPoint PPT presentation

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Title: NCSU MAE


1
Leading-Edge Flame Oscillations in Lifted
Turbulent Flames
Nancy Moore Advisor Dr. Kevin Lyons
  • Effective Velocity
  • Equation better relates the lifted height to the
    flow velocities than the Reynolds number.
  • Ueff, U0, and Ucf are the effective, fuel, and
    co-flow velocities, respectively, and ?cf / ?0 is
    the ratio of the co-flow to fuel densities.
  • The constant C is chosen such that the data
    collapses to a linear relation.
  • Introduction
  • In numerous industrial applications such as
    furnaces and burners, the location of the flame
    base and thus the location of the maximum heat
    release is an important design element.
  • By increasing the fuel or co-flow velocity, an
    attached flame will lift off the nozzle and
    stabilize at a mean lifted height, with a
    tendency to oscillate axially about that mean
    position.
  • The reaction zone lifted-height oscillations are
    studied to shed light on the stabilization
    mechanisms that prevent flames from receding
    downstream and extinguishing.
  • Various combinations of fuel and co-flow
    velocities (2,800 Re 10,700) are used to
    study lifted flames at a wide range of downstream
    locations for two different nozzle diameters.

Oscillatory Behavior of Flame in Sequenced Images
with Average Height of 3.12 cm ?t 1/30 sec,
Fuel Velocity 22.6 m/s, Co-Flow Velocity 0.0
m/s, d 3.5 mm
  • Rate of Oscillations
  • The oscillatory rate, dh'/dt, uses a lab frame of
    reference and is positive for downstream
    recession.
  • Because the radial flame position was not noted
    with the height, dh'/dt has only an axial
    component.

h' 3.87 cm
h' 3.87 cm
h' 3.39 cm
h' 3.14 cm
h' 2.78 cm
h' 3.27 cm
h' 4.11 cm
h' 4.11 cm
  • Average Heights for d 3.5 mm
  • Height increases with fuel velocity and with
    co-flow velocity.
  • Error bars represent maximum height fluctuations
    seen upstream and downstream.
  • Although the fluctuation magnitude increases with
    downstream location, it is reduced in
  • the presence
  • of co-flow.
  • Similar
  • trends are
  • seen in
  • the data
  • from
  • d 5.0 mm
  • (not shown).
  • Height Fluctuations Normalized by the Average
    Height
  • The greatest downstream h' (marked by a solid
    symbol) and the greatest upstream
  • h' (marked by a symbol outline) for each case are
    shown.
  • Oscillation fluctuations are not generally
    symmetric about the average height.
  • For flames stabilized at h fluctuations
  • are generally above 0.3h.
  • Downstream of this region, the turbulence can be
    assumed to
  • be fully developed.
  • For h 10d, the oscillation behavior is more
    uniform with data
  • showing h' 0.3h.
  • Approaching blowout (h 35d) the normalized
    fluctuations
  • are not significantly greater except for the case
    with no co-flow
  • present.
  • The ratio h'/h does not significantly change with
    nozzle
  • diameter.
  • Experimental Setup
  • Methane (99 pure) delivered through fuel tubes
    of 3.5 mm or 5.0 mm inner diameter, d (measured
    by a rotameter).
  • Co-flow air annulus has 150 mm diameter (measured
    by a TSI velocimeter).
  • Images of the oscillating flame were made with a
    Panasonic Model PV-GS300 CCD video camera
    producing thirty frames per second.
  • The instantaneous flame height, h', is the axial
    distance from the nozzle exit to the flame base,
    which is the furthest point upstream at which
    flame luminosity is detected by the camera.
  • Conclusions
  • Though much smaller than the fuel velocity, the
    co-flow velocity significantly affects the
    location and behavior of a flame.
  • The flame height, fluctuations, and oscillatory
    rate are related to the flow velocities.
  • The average height increases with fuel and with
    co-flow velocity.
  • The nozzle diameter is inversely related to the
    lifted height but has little affect on the
    normalized fluctuations.
  • Height fluctuations increase with height and are
    reduced in the presence of co-flow,
    while
  • Normalized Height Plotted With Re and Ueff
  • For a given Reynolds number, the larger nozzle
    results in lower lifted heights.
  • The height change with Reynolds number is linear
    for the majority of cases, with exceptions at the
    upper and lower limits.
  • Setting C 40 in Ueff collapses the data to a
    linear relation.

Aperiodic Behavior of Oscillations Co-Flow
Velocity 0.0 m/s, d 3.5 mm
  • RMS of Oscillatory Rate
  • d 3.5 mm
  • Setting C 5.2 in Ueff collapses the data to a
    linear relation.
  • for d 5.0 mm, C 15 (not shown)
  • Also, the oscillatory rate is not strongly
    correlated with height.
  • increases with the average height
  • less at a given height when co-flow is present,
    suggesting that the presence of co-flow has a
    greater affect on the oscillatory rate throughout
    the entire flowfield than it does on the
    normalized fluctuations
  • normalized height fluctuations show little
    variation with height except at locations close
    to the
  • nozzle or approaching blowout far downstream.
  • Plotting the height and oscillatory rate with the
    effective velocity collapses the data into a
    linear relation. However, different values of C
    are needed.
  • C 40 for height and d 3.5 mm or d 5.0 mm
  • C 5.2 for oscillatory rate and d 3.5 mm
  • C 15 for oscillatory rate and d 5.0 mm
  • Montgomery et al. (1998) speculated that the
    constant, C, in the effective velocity equation
    takes into account chemical kinetics and burner
    characteristics.
  • Results imply that the largest scales of
    turbulence influencing the lifted height do not
    play a primary role in the oscillation behavior.

Acknowledgement This research has been
supported by the U. S. Army Research Office
(Contract W911NF0510045).
NC STATE UNIVERSITY
MECHANICAL AND AEROSPACE ENGINEERING
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