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Transport equation for the isotropic turbulent energy dissipation rate in the far-wake of a circular cylinder

机译:圆柱远场中各向同性湍流能量耗散率的输运方程

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The transport equation for the isotropic turbulent energy dissipation rate (epsilon) over bar (iso) along the centreline in the far-wake of a circular cylinder is derived by applying the limit at small separations to the two-point energy budget equation. It is found that the imbalance between the production and the destruction of (epsilon) over bar (iso), respectively due to vortex stretching and viscosity, is governed by both the streamwise advection and the lateral turbulent diffusion (the former contributes more to the budget than the latter). This imbalance differs intrinsically from that in other flows, e.g. grid turbulence and the flow along the centreline of a fully developed channel, where either the streamwise advection or the lateral turbulent diffusion of (epsilon) over bar (iso) governs the imbalance. More importantly, the different types of imbalance represent different constraints on the relation between the skewness of the longitudinal velocity derivative S and the destruction coefficient of enstrophy G. This results in a non-universal approach of S towards a constant value as the Taylor microscale Reynolds number R-lambda increases. For the present flow, the magnitude of S decreases initially (R-lambda <= 40) before increasing (R-lambda > 40) towards this constant value. The constancy of S at large R-lambda violates the modified similarity hypothesis introduced by Kolmogorov (J. Fluid Mech., vol. 13, 1962, pp. 82-85) but is consistent with the original similarity hypotheses (Kolmogorov, Dokl. Akad. Nauk SSSR, vol. 30, 1941b, pp. 299-303 (see also 1991 Proc. R. Soc. Lond. A, vol. 434, pp. 9-13)) (K41), and, more importantly, with the almost completely self-preserving nature of the plane far-wake.
机译:通过将小间距上的极限值应用于两点能量收支方程,得出圆柱的苏醒时各向同性湍流能量耗散率(ε)沿中心线在横条(iso)上的输运方程。研究发现,由于涡流拉伸和粘性,分别在棒(iso)上产生和破坏(ε)之间的不平衡是由流向平流和横向湍流扩散共同控制的(前者对预算的贡献更大)比后者)。这种不平衡本质上不同于其他流程中的不平衡,例如网格湍流和沿充分发展的通道中心线的流动,其中流向对流或(ε)在横条(iso)上的横向湍流扩散控制着不平衡。更重要的是,不同类型的失衡对纵向速度导数S的偏度和涡旋G的破坏系数之间的关系表示了不同的约束。这导致了S朝着恒定值的非通用方法,如泰勒微尺度雷诺兹R-lambda数增加。对于当前的流量,S的大小先朝(R-lambda> = 40)减小,然后朝该恒定值增大(R-lambda> 40)。大Rλ处S的恒定性违反了Kolmogorov提出的修正的相似性假设(J. Fluid Mech。,第13卷,1962年,第82-85页),但与原始相似性假设(Kolmogorov,Dokl。Akad)一致Nauk SSSR,第30卷,1941b,第299-303页(另请参见1991 Proc。R. Soc。Lond。A,第434卷,第9-13页)),并且更重要的是,这架飞机几乎完全是自我保护的。

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