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Turbulent Flow Produced by Piston Motion in a Spark-ignition Engine

机译:火花点火发动机中活塞运动产生的湍流

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摘要

Turbulence produced by the piston motion in spark-ignition engines is studied by 2D axisymmetric numerical simulations in the cylindrical geometry as in the theoretical and experimental work by Breuer et al. (Flow Turbul Combust 74:145, 2005). The simulations are based on the Navier–Stokes gas-dynamic equations including viscosity, thermal conduction and non-slip at the walls. Piston motion is taken into account as a boundary condition. The turbulent flow is investigated for a wide range of the engine speed, 1,000–4,000 rpm, assuming both zero and non-zero initial turbulence. The turbulent rms-velocity and the integral length scale are investigated in axial and radial directions. The rms-turbulent velocity is typically an order-of-magnitude smaller than the piston speed. In the case of zero initial turbulence, the flow at the top-dead-center may be described as a combination of two large-scale vortex rings of a size determined by the engine geometry. When initial turbulence is strong, then the integral turbulent length demonstrates self-similar properties in a large range of crank angles. The results obtained agree with the experimental observations of Breuer et al. (Flow Turbul Combust 74:145, 2005).
机译:由Breuer等人的理论和实验工作,通过圆柱几何中的二维轴对称数值模拟研究了火花点火发动机中活塞运动产生的湍流。 (Flow Turbul Combust 74:145,2005)。模拟基于Navier-Stokes气体动力学方程式,包括黏性,导热性和壁面防滑性。活塞运动被视为边界条件。在假定初始湍流为零和非零的情况下,研究了发动机转速在1,000-4,000 rpm的宽范围内的湍流。在轴向和径向方向研究了湍流的均方根速度和积分长度标尺。均方根湍流速度通常比活塞速度小一个数量级。在初始湍流为零的情况下,上止点处的流动可描述为两个大型涡流环的组合,其大小由发动机几何形状确定。当初始湍流很强时,整体湍流长度会在很大的曲柄角范围内表现出自相似的特性。得到的结果与Breuer等人的实验观察结果一致。 (Flow Turbul Combust 74:145,2005)。

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