2017
DOI: 10.1515/bfuel-2017-0005
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Combustion Characteristics and Laminar Flame Speed of Premixed Ethanol-Air Mixtures with Laser-Induced Spark Ignition

Abstract: Laser-induced spark-ignition (LISI) has an advanced ignition technique with a few benefits over spark ignition. In this study, flame morphology, laminar flame characteristics and combustion characteristics of premixed anhydrous ethanol and air mixtures were investigated using LISI generated by a Q-switched Nd: YAG laser (wavelength: 1064 nm). Experiments were conducted in a constant volume combustion chamber (CVCC) at the initial condition of T0=358 K and P0=0.1 MPa, respectively, and with equivalence ratios (… Show more

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Cited by 7 publications
(4 citation statements)
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“…Flame propagation is also related to the compression ratio, for example the greater the compression ratio, the higher the flame propagation speed [27]. Thus the use of bioefuels makes it possible to increase the compression ratio in gasoline engines, without the problem of knocking and accelerating flame propagation, on the other hand flame propagation is not affected by the ignition method, which is a characteristic of biofuel-air mixtures [28]. Flame instability also plays a role in performance and emission results.…”
Section: Literature Reviewmentioning
confidence: 99%
“…Flame propagation is also related to the compression ratio, for example the greater the compression ratio, the higher the flame propagation speed [27]. Thus the use of bioefuels makes it possible to increase the compression ratio in gasoline engines, without the problem of knocking and accelerating flame propagation, on the other hand flame propagation is not affected by the ignition method, which is a characteristic of biofuel-air mixtures [28]. Flame instability also plays a role in performance and emission results.…”
Section: Literature Reviewmentioning
confidence: 99%
“…In these equations, ∇ denotes the tangential gradient operator, → u is the fluid velocity, → u vertex is the velocity of the moving vertex, while ρ u and ρ b represent the average densities of the unburned and burned mixtures, respectively. The term D T is the turbulent diffusivity, κ is the Favre mean flame front curvature, and C S , a 4 , b 1 , and b 3 are model constants provided in [8,12,35,36]. The quantities k and ε are the Favre mean turbulent kinetic energy and its dissipation rate from the RNG k − ε model, while u is the turbulence velocity fluctuation.…”
Section: Turbulent Flame Speedsmentioning
confidence: 99%
“…The quantities k and ε are the Favre mean turbulent kinetic energy and its dissipation rate from the RNG k − ε model, while u is the turbulence velocity fluctuation. The turbulent flame S O T , used in the G-equation, is obtained through the following equation [8,12,35,36]:…”
Section: Turbulent Flame Speedsmentioning
confidence: 99%
“…Among these, rapid compression machines (RCM) [2][3][4][5], shock tubes (ST) [6][7][8][9][10] or both [11][12][13][14][15] are the most widespread. A qualitative description of the self-ignition delay is given in Figure 1 as a plot pressure P or radiation intensity RI in time: The forced ignition, particularly spark ignition, sometimes supplemented with plasma or laser [15][16][17][18][19][20], was frequently studied using constant volume combustion bombs (CVB). The method presented in this paper relies on the analysis of the radiation intensity variation during the early stages of spark ignition in a CVB.…”
Section: Introductionmentioning
confidence: 99%