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Modelling of Combustion-Chamber Film-Coolant Flow in Rocket Engines

机译:火箭发动机燃烧室薄膜冷却剂流动的建模

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The main purpose of this study is to investigate film instability and hence the entrainment mechanisms of the liquid film of cooling flow by computational fluid dynamics (CFD) techniques. In the modelling, a two-layer k-ε turbulence model is used with a high Reynolds number k-ε turbulence model away from the walls while the near-wall viscosity-affected layer is resolved with a one-equation model. So as to accommodate the two-phase interface, the Scalar Equation (Volume of Fluid) Method was used. In addition to the investigation of entrainment mechanisms, the nature of the film-coolant released into the atmosphere, with and without chemistry (combustion) included is examined. The transient numerical simulations indicate the generation of disturbance waves at the liquid-gas interface for coolant flows above a critical value and their growth result in liquid entrainment. The film-coolant flow was found to persist into the wake, which has environmental implications, in that if afterburning is not used, then cracked large-molecule hydrocarbons are then the primary product instead of soot formation.
机译:这项研究的主要目的是通过计算流体动力学(CFD)技术研究膜的不稳定性,从而研究冷却流液膜的夹带机理。在建模中,使用两层k-ε湍流模型,并使用远离壁的高雷诺数k-ε湍流模型,而近壁粘度影响层通过单方程模型求解。为了容纳两相界面,使用了标量方程(流体体积)方法。除了研究夹带机制外,还检查了释放到大气中的薄膜冷却剂的性质,包括和不包括化学物质(燃烧)。瞬态数值模拟表明,在液-气界面处,对于高于临界值的冷却液流量会产生扰动波,并且扰动波的增长会导致夹带液体。发现薄膜冷却剂流持续存在于尾流中,这对环境具有影响,因为如果不使用后燃,则裂化的大分子碳氢化合物将成为主要产物,而不是形成烟灰。

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