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A hybrid asymptotic-numerical method for calculating drag coefficients in 2-D low Reynolds number flows

机译:二维低雷诺数流中阻力系数的混合渐近数值方法

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摘要

Steady-state incompressible low-Reynolds-number fluid flow past a cylindrical body in an unbounded two-dimensional domain is a singular perturbation problem involving an infinite logarithmic expansion in the Reynolds number ε as ε → 0. The central difficulty with applying a conventional matched asymptotic approach to this problem is that only the first few terms in the infinite logarithmic expansion of the drag coefficient and of the flow field can be calculated analytically. To overcome this difficulty, a hybrid asymptotic-numerical method that incorporates all logarithmic correction terms is implemented for three low-Reynolds-number flow problems. In particular, for a nanocylinder of circular cross section with surface roughness, modeled by a Navier boundary condition involving a sliplength parameter, a hybrid asymptotic-numerical method is formulated and implemented to determine an approximation to the drag coefficient that is accurate to all powers of - 1/ log ε. A similar analysis is done to determine a corresponding approximation of the drag coefficient for a porous cylinder, where the flow inside the cylinder is modeled by the Brinkman equation. For both the nano- and porous-cylinder problems, the hybrid asymptotic-numerical method is extended to calculate the first transcendentally small correction term to the Stokes flow near a body. This term, which governs weak upstream/downstream asymmetry in the Stokes flow, is extrapolated to finite ε to predict the formation of any eddies near the body. Finally, the hybrid method is used to determine the drag coefficient, valid to within all logarithmic terms, for two identical cylinders of circular cross section in tandem alignment with the free stream. An extension of the theoretical framework to more general slow viscous flow problems is discussed.
机译:稳态不可压缩的低雷诺数流体在无界二维域中流过圆柱体是一个奇异的摄动问题,涉及到雷诺数ε为ε→0的对数无限扩展。应用传统匹配方法的主要困难该问题的渐近方法是,只能解析地计算阻力系数和流场的无限对数展开中的前几项。为了克服这一困难,针对三个低雷诺数流动问题,采用了一种包含所有对数校正项的混合渐近数值方法。特别是,对于具有表面粗糙度的圆形横截面的纳米圆柱体,通过涉及滑动长度参数的Navier边界条件建模,制定了混合渐近数值方法,并确定了对阻力系数的近似值,该近似值适用于所有幂次方。 -1 /对数ε。进行了类似的分析来确定多孔圆柱体的阻力系数的相应近似值,其中圆柱体内部的流动由Brinkman方程建模。对于纳米圆柱体和多孔圆柱体这两个问题,混合渐近数值方法得到扩展,可以计算出人体附近斯托克斯流的第一个超验小校正项。控制斯托克斯流中上游/下游弱对称性的该项外推至有限ε,以预测人体附近任何涡流的形成。最后,使用混合方法来确定在两个对数项内有效的,与自由流串联排列的两个相同圆形截面圆柱体的阻力系数。讨论了将理论框架扩展到更一般的慢粘性流动问题。

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