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NUMERICAL MODELING OF GASEOUS PARTIALLY PREMIXED LOW-SWIRL LIFTED FLAME AT ELEVATED PRESSURE

机译:升压气体部分预混的低旋风提升火焰的数值模拟

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Lifted flames have been investigated in the past years for their benefits in terms of NO_x emissions reduction for gas turbine applications. In a lifted flame, the flame front stabilized on a position that is significantly detached from the nozzle exit, improving the premixing process before the reaction zone. The distance between the flame front and the nozzle exit is called liftoff height and it represents the main parameter that characterize this type of flame. In the present work, a partially premixed lifted flame employing air-methane mixture is investigated through numerical simulation. Indeed, even if lifted jet flames have been widely studied in the literature, there are only a few examples of lifted partially premixed flames. Nevertheless, this kind of flames assumes an important role considering the current gas turbine applications, since their benefits in terms of stability and low pollutant emissions. This study has been performed with LES calculations using a commercial software suite and the numerical results are compared with experimental data coming from a dedicated campaign held at Karlsruher Institute fuer Technologie (KIT) on a novel low-swirl injector nozzle. Quenching effects due to strain, curvature and heat loss have been introduced into the combustion model thanks to a correction of the source term in the progress variable equation within the FGM model. The comparison between numerical results and experimental data have been performed in terms of lift-off height and OH* chemilumi-nescence maps, showing the capability to properly predict the overall flow and to catch flame lift-off even if with an underpre-dicted height. This points out promising capability of the numerical model in the representation of lifted flames, allowing further investigations of the flame structure otherwise not available from experimental techniques.
机译:解除火焰在过去几年追究其好处NO_x的减排燃气轮机应用方面。在提升的火焰,火焰前缘稳定在所显著从喷嘴出口脱离的位置时,所述反应区之前提高预混合过程。火焰前缘和喷嘴出口之间的距离被称为剥离的高度和它代表表征这种类型的火焰的主要参数。另外,在本工作中,采用空气 - 甲烷混合物的部分预混合火焰解除通过数值模拟研究。事实上,即使解除喷射火焰已被广泛研究在文献中,只有解除部分预混火焰的几个例子。然而,这种火焰的假设考虑到目前的燃气涡轮机应用的重要作用,因为它们在稳定性和低污染物排放方面的好处。这项研究已使用商业软件套件和数值结果与从卡尔斯鲁厄研究所附耳TECHNOLOGIE(KIT)一种新型低漩涡喷油嘴举行了专门的广告的实验数据来比较LES计算执行。由于应变,曲率和热损失淬火效应已被引入到燃烧模型得益于FGM模型内的进展变量方程中的源项的校正。数值结果和实验数据之间的比较已经在剥离高度和OH * chemilumi-nescence图,示出了该能力正确地预测的总体流动并捕获火焰方面已经进行剥离,即使有underpre-dicted高度。这点有前途的数值模型的能力,提升火焰的表现,使火焰结构,否则无法从实验技术的进一步调查。

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