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Opposed Jet Burner Extinction Limits: Simple Mixed Hydrocarbon Scramjet Fuels vs Air

机译:反对的喷气式燃烧器消光极限:简单的混合碳氢超燃冲压燃料与空气

摘要

Opposed Jet Burner tools have been used extensively by the authors to measure Flame Strength (FS) of laminar non-premixed H2 air and simple hydrocarbon (HC) air counterflow diffusion flames at 1-atm. FS represents a strain-induced extinction limit based on air jet velocity. This paper follows AIAA-2006-5223, and provides new HC air FSs for global testing of chemical kinetics, and for characterizing idealized flameholding potentials during early scramjet-like combustion. Previous FS data included six HCs, pure and N2-diluted; and three HC-diluted H2 fuels, where FS decayed very nonlinearly as HC was added to H2, due to H-atom scavenging. This study presents FSs on mixtures of (candidate surrogate) HCs, some with very high FS ethylene. Included are four binary gaseous systems at 300 K, and a hot ternary system at approx. 600 K. The binaries are methane + ethylene, ethane + ethylene, methane + ethane, and methane + propylene. The first three also form two ternary systems. The hot ternary includes both 10.8 and 21.3 mole % vaporized n-heptane and full ranges of methane + ethylene. Normalized FS data provide accurate means of (1) validating, globally, chemical kinetics for extinction of non-premixed flames, and (2) estimating (scaling by HC) the loss of incipient flameholding in scramjet combustors. The n-heptane is part of a proposed baseline simulant (10 mole % with 30% methane + 60% ethylene) that mimics the ignition of endothermically cracked JP-7 like kerosene fuel, as suggested by Colket and Spadaccini in 2001 in their shock tube Scramjet Fuels Autoignition Study. Presently, we use FS to gauge idealized flameholding, and define HC surrogates. First, FS was characterized for hot nheptane + methane + ethylene; then a hot 36 mole % methane + 64% ethylene surrogate was defined that mimics FS of the baseline simulant system. A similar hot ethane + ethylene surrogate can also be defined, but it has lower vapor pressure at 300 K, and thus exhibits reduced gaseous capacity. The new FS results refine our earlier idealized reactivity scale that shows wide ranging (50 x) diameter-normalized FSs for various HCs. These range from JP-10 and methane to H2 air, which produces an exceptionally strong flame that agrees within approx. 1% of recent 2-D numerically simulations. Finally, we continue advocating the FS approach as more direct and fundamental, for assessing idealized scramjet flameholding potentials, than measurements of unstrained laminar burning velocity or blowout in a Perfectly Stirred Reactor.
机译:作者已广泛使用对置的Jet Burner工具来测量层状非预混合H2空气的火焰强度(FS)和1-atm的简单碳氢化合物(HC)空气逆流扩散火焰。 FS表示基于空气喷射速度的应变诱发的消光极限。本文遵循AIAA-2006-5223,并提供了新的HC空气FS,用于全球化学动力学测试,以及在早期超燃冲压式燃烧过程中表征理想的阻焰潜力。先前的FS数据包括六种纯净和N2稀释的HC。以及三种HC稀释的H2燃料,其中由于H原子的清除,当HC加入H2时,FS非线性地衰减。这项研究提出了(候选替代物)HC混合物中的FS,其中有些具有很高的FS乙烯。包括四个300 K的二元气态系统和一个约200 K的热三元系统。 600K。二元是甲烷+乙烯,乙烷+乙烯,甲烷+乙烷和甲烷+丙烯。前三个还形成两个三元系统。热三元包括10.8和21.3摩尔%的汽化正庚烷以及全部范围的甲烷+乙烯。标准化的FS数据提供了以下精确方法:(1)总体上验证非预混火焰熄灭的化学动力学,以及(2)估计超燃式燃烧器中初期火焰保持的损失(通过HC缩放)。正庚烷是拟议的基准模拟物(10摩尔%,含30%甲烷+ 60%乙烯)的一部分,该模拟物模拟了吸热裂化的JP-7(如煤油燃料)的点燃,这是Colket和Spadaccini在2001年在其冲击管中提出的超燃冲压燃料自动点火研究。目前,我们使用FS来衡量理想化的火焰稳定度,并定义HC替代物。首先,FS的特征是热庚烷+甲烷+乙烯;然后定义了热的36摩尔%的甲烷+ 64%的乙烯替代物,该模拟物可模拟基准模拟系统的FS。也可以定义类似的热乙烷+乙烯替代物,但在300 K时蒸汽压较低,因此显示出较低的气态容量。新的FS结果完善了我们较早的理想反应活性标度,该标度显示了各种HC的宽范围(50 x)直径归一化FS。范围从JP-10和甲烷到H2空气,会产生异常强烈的火焰,在大约10分钟内达到一致。最近的2D数值模拟的1%。最后,与在完全搅拌反应堆中无应变层流燃烧速度或井喷的测量相比,我们继续主张采用FS方法更为直接和基本,以评估理想的超燃冲压火焰潜力。

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