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The burning rate is essential for the determination of flame temperatures, flame lengths, and burnout, all critical parameters to establish fire growth.
It is expected that the ability to predict flame behavior near such singular points will be particularly useful in the determination of flame kinetics.
Thermocouple is used for the determination of flame temperature, velocity measurement is made using particle image velocimetry (PIV), and the flame front position is measured by direct photograph as well as with laser-induced predissociative fluorescence (LIPF) of OH imaging techniques.
The flame diagnostics consist of one-dimensional (1-D) Planar Laser-Induced Fluorescence (PLIF) for measurements of NO and CH concentrations, 1-D NO-LIF thermometry, and 1-D Particle Tracking Velocimetry (PTV) for the determination of flame reactivity and burning rates.
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Despite the high turbulence levels in the combustor, signals were obtained on virtually every laser shot, and these signals were strong enough for spectral fitting analysis for determination of flames temperatures.
The simulation was performed for one dimensional, planar, premixed flames for determination of laminar flame speeds, as well as for the opposed jet, strained, laminar premixed and non-premixed flames for the determination of extinction strain rates.
The effect of nonspherical (i.e. cylindrical) bomb geometry on the evolution of outwardly propagating flames and the determination of laminar flame speeds using the conventional constant-pressure technique is investigated experimentally and theoretically.
The accuracy of the counterflow, twin-flame technique for the determination of laminar flame speeds was examined analytically, numerically and experimentally.
The simulations were carried out for counterflow and spherically expanding flames given that both configurations are used extensively for the determination of laminar flame speeds.
Using the propagating spherical flame, we assessed the impact of two-stage heat release on the determination of laminar flame speed.
This is the case for Le<1 flames, with the most notable example being ultralean H2/air flames, which develop cellular structures at low strain rates so that determination of laminar flame speeds for such mixtures is not possible.
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