首页> 外文会议>AIAA 33rd Aerospace Seicnces Meeting and Exhibit January 9-12, 1995/Reno, NV >Simulation of the reacting field in an axisymmetric bluff-body combustor using the vortex-scalar element method-an isothermal, fast-chemistry model
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Simulation of the reacting field in an axisymmetric bluff-body combustor using the vortex-scalar element method-an isothermal, fast-chemistry model

机译:轴对称钝体燃烧室中反应场的涡量标量法-等温快速化学模型的模拟

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Axisymmetric, time-dependent simulations are performed for a binary, single-step chemically reacting flow in a two-stream, coaxial-jet bluff-body combustor using the Lagrangian vortex-scalar element method in order to study the effect of the large-scale eddies on the mixing and the rate of product formation in the recirculation region behind the bluff body. The method solves the unaveraged time-dependent governing equations by discretizing the vorticity and the scalar field using a number of finite-area vortext and scalar ring elements, respectively. Simulations have been performed at three flow conditions: the annular-flow dominated regime, U_j/U_a chemical bounds 0.62; the transition regime, U+j/U_a chemical bounds 1.04; and the jet dominated regime, U_j/U_a chemical bounds 2.08. In agreement with experimental studies, our simulations show that when the annular flow dominates the field, a short, compact flame is confined to the recirculation rgion with quasi periodic shedding of large packetws of reacting fluid from the recirculation zone. In the transition regime where the velocity of the jet and the annular flow are approximately equal, an intermittient pulsating flame with a reaction zone attached to the bluff body is observed. In the jet dominated regime, the flow experimences much less flutuation and entrainment, and most of the jet fluid is confined to a narrow region close to the centerline where mixing and reaction are most intense. The simulations also reveal that regardless of the velocity ratio, products are found mostly in regions associated with the large-scale vortical structures located on the outskirts of the shear region defined by these structures. The time-averaged product distribution, consistent with experimental results, shows lower overall concentration and is free of local hot spots due to the cyclical nature of the flow field. However, the unsteady field exhibits local hot s pots where the product mass fraction is unity.
机译:使用拉格朗日涡旋标量元素方法对两流同轴射流钝体燃烧器中的二元单步化学反应流进行轴对称,与时间有关的模拟,以研究大规模效应在钝体后方的回流区域中,对混合和产物形成的速率产生涡流。该方法通过分别使用多个有限区域的vortext和标量环元素离散涡度和标量场来求解非平均时间相关的控制方程。在三种流动条件下进行了模拟:环形流动占主导的状态,U_j / U_a化学范围为0.62;过渡态,U + j / U_a化学范围1.04;和喷射主导的体制,U_j / U_a化学界为2.08。与实验研究一致,我们的模拟结果表明,当环形流主导该场时,一个短而紧凑的火焰被限制在再循环区域内,并且周期性周期性地散发大量来自反应区的反应流体。在射流速度和环形流的速度大致相等的过渡状态下,观察到间歇性脉动火焰,其反应区附着在阻流体上。在喷射为主的状态下,流动的波动和夹带少得多,并且大多数喷射流体被限制在靠近中心线的狭窄区域,在该中心线混合和反应最激烈。模拟还表明,无论速度比如何,都主要在与大型旋涡结构相关的区域中找到产物,这些大型旋涡结构位于这些结构所定义的剪切区域的郊区。与实验结果一致的时间平均产品分布显示出较低的总浓度,并且由于流场的周期性而没有局部热点。但是,不稳定区域会出现局部火锅,其中产品质量分数是统一的。

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