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Experimental investigation of the flame extinction processes of nonpremixed methane flames inside an air coflow diluted with CO_2, N_2, or Ar

机译:用CO_2,N_2或Ar稀释的气流中非预混甲烷火焰熄灭过程的实验研究

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The flame extinction processes and lifted flame stabilization features of nonpremixed flames issuing in diluted coflowing air were systematically examined under a wide range of aerodynamic conditions in order to reveal the competition between aerodynamics and dilution. Four diluents (CO_2, N_2, Ar, and CO_2 + Ar) were used in preparation for discriminating between the effects, namely, dilution, thermal action, and chemistry, induced by diluent addition. Flame extinction limits, ignition diagrams, liftoff height, and its associated apparent radius were investigated to provide key elements involved in lifted flame stabilization and extinction mechanisms with a diluted air stream. Flame extinction limits have been expressed as a 3D surface E_(extinction) in the physical space (Q_(diluent)/Q_(air), U_(air), U_(CH4). This surface is composed of two parts, a pure extinction surface where flame extinction is necessarily attained from lifted flames, and a common surface between flame lifting and extinction where flame extinction is achieved directly from attached flames. This distinct behavior is due to the presence of the semithick burner rim that protects the flame base. The flame ignition diagrams confirm that the pure extinction surface is independent of U_(CH4) for flames initially lifted without dilution. Furthermore, (Q_(diluent)/Q_(air))/K_(diluent), where K_(diluent) characterizes the capacity of a diluent to act on the flame destabilization process, has proved to be the affine parameter leading to a unified extinction surface for the tested chemically weak diluents. Moreover, by using (Q_(diluent)/Q_(air))/K_(diluent). liftoff height H_L/H_L~o and flame radius R_P/R_P~o reduced by the no-dilution measures merge to unique self-similar curves whatever the diluents and aerodynamic conditions. The key element is the flame leading-edge burning velocity, which was found to be identical for diluted flames when the diluents were added into the air stream in the relative proportions given by K_(diluent). In this way, it is possible to estimate flame behavior based on the results for CO_2, once K_(diluent) is known.
机译:在广泛的空气动力学条件下,系统地研究了稀释的同流空气中非预混火焰的熄灭过程和增强的火焰稳定特性,以揭示空气动力学与稀释之间的竞争。制备中使用了四种稀释剂(CO_2,N_2,Ar和CO_2 + Ar)来区分稀释剂添加引起的效应,即稀释,热作用和化学作用。研究了熄火极限,点火图,升空高度及其相关的视在半径,以提供与稀薄空气流有关的提升的火焰稳定和熄灭机制的关键要素。消光极限表示为物理空间(Q_(稀释剂)/ Q_(空气),U_(空气),U_(CH4)中的3D表面E_(消光)。该表面由两部分组成,一个是纯消光必须通过抬升的火焰实现熄火的表面,以及在火焰升起和熄灭之间的共同表面,在该表面直接通过附着的火焰实现熄火,这种不同的行为是由于存在了保护火焰根的半厚燃烧器边缘。火焰点火图证实,最初消散的火焰的纯消光表面与U_(CH4)无关,此外,(Q_(稀释剂)/ Q_(空气))/ K_(稀释剂),其中K_(稀释剂)表征了容量稀释剂在火焰稳定过程中的作用,被证明是仿射参数,可导致被测试的化学弱稀释剂具有统一的消光表面,此外,使用(Q_(稀释剂)/ Q_(空气))/ K_(稀释剂)。升空高度H_L / H_L〜o和火焰弧度无论稀释剂和空气动力学条件如何,通过无稀释措施降低的R_P / R_P〜o合并为唯一的自相似曲线。关键因素是火焰前沿燃烧速度,当以K_(稀释剂)给定的相对比例将稀释剂添加到空气流中时,稀释火焰的燃烧速度是相同的。这样,一旦知道K_(稀释剂),就可以根据CO_2的结果估算火焰行为。

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