Simultaneous visualization of instantaneous unburnt and preheating zones in turbulent premixed flames under transverse acoustic excitations

Abstract

Instantaneous unburnt and preheating zones of bluff-body stabilized turbulent methane-air premixed flames under transverse acoustic excitations were investigated using simultaneous planar laser-induced fluorescence (PLIF) of acetone and CH2O, as well as multi-point hot-wire measurements. The PLIF images show that the unburnt zone marked by acetone, the preheating zone marked by CH2O, and the pixel-by-pixel product of acetone/CH2O have an increasing distribution area when slowly enlarging the sound pressure level (SPL). Wrinkled and bent edges of the unburnt and preheating zone can be seen at conditions away from the flame blow-off in the presence of the transverse acoustic excitations, and their sizes and areas increase as the flame blow-off is approached. At conditions near the flame blow-off with enlarging SPL to 123 dB, the flame turns from side to side over time and a large scale of the acetone/CH2O regions can be observed to deflect inside the center product zone, implying that the cold reactants enter into the product zone from the unburnt/preheating zones. The unburnt/preheating mainstream presents strong wrinkles, and partial areas occurred some fractures. Such a phenomenon indicates that the local extinction of the shear layer flame can also be facilitated due to the turbulent fluctuation enhanced by the transverse acoustic wave. For a low flow velocity, increasing variations of the unburnt and preheating zones in the presence of the transverse acoustic wave was revealed. The curvature of the acetone PLIF showed that the unburnt zones were more likely to be wrinkled with an increasing SPL and flow velocity.

Investigation of dynamic mixedness characteristics of a transverse acoustically excited turbulent jet by high-repetition-rate acetone tracer planar laser-induced fluorescence technique

“…The jet turbulence intensity rises with the whole RMS velocity, including the RMS velocities of the ow and acoustic wave. When the ow outlet velocity decreases, the ow RMS velocity decreases, and the acoustic RMS velocity dominates the entire RMS velocity (Yan et al 2022). Therefore, larger changes can be observed in the lower velocity ow.…”

“…The jet velocities varied from 4.71 m/s to 13.20 m/s, providing Reynolds (Re) numbers of 2000-5600. The Re number was calculated using the formula (Li et al 2010;Yan et al 2022), where , U, and represent the density, velocity, and viscosity coe cient of the mixture, respectively. The hydraulic diameter D 0 = 2(r 1 − r 0 ) was used as the characteristic length D when computing Re.…”

Quantitative acetone/toluene planar laser‐induced fluorescence measurements of equivalent ratio

“…PLIF technology is widely used in combustion field diagnostics,[48][49][50] but acetone/toluene PLIF technique cannot be directly applied to the measurement of equivalence ratio in combustion fields. However, we can use OH-PLIF technology to verify the reliability of the acetone/toluene PLIF technique's measurement results in combustion fields.…”