NASA Glenn Research Center, 2100 Brookpark Road, Cleveland, 44135 OH, USA
Philos Trans A Math Phys Eng Sci. 2014 Jul 28;372(2020). doi: 10.1098/rsta.2013.0354.
This paper is concerned with the transition to turbulence in flat plate boundary layers due to moderately high levels of free-stream turbulence. The turbulence is assumed to be generated by an (idealized) grid and matched asymptotic expansions are used to analyse the resulting flow over a finite thickness flat plate located in the downstream region. The characteristic Reynolds number Rλ based on the mesh size λ and free-stream velocity is assumed to be large, and the turbulence intensity ε is assumed to be small. The asymptotic flow structure is discussed for the generic case where the turbulence Reynolds number εRλ and the plate thickness and are held fixed (at O(1) and O(λ), respectively) in the limit as [Formula: see text] and ε→0. But various limiting cases are considered in order to explain the relevant transition mechanisms. It is argued that there are two types of streak-like structures that can play a role in the transition process: (i) those that appear in the downstream region and are generated by streamwise vorticity in upstream flow and (ii) those that are concentrated near the leading edge and are generated by plate normal vorticity in upstream flow. The former are relatively unaffected by leading edge geometry and are usually referred to as Klebanoff modes while the latter are strongly affected by leading edge geometry and are more streamwise vortex-like in appearance.
本文研究了由于中等强度的自由流湍流引起的平板边界层向湍流的转变。假设湍流是由(理想化的)格栅产生的,并且使用匹配渐近展开来分析位于下游区域的有限厚度平板上的流动。基于网格尺寸 λ 和自由流速度的特征雷诺数 Rλ 被假定为大,并且假定湍流强度 ε 为小。渐近流动结构对于一般情况进行了讨论,其中在[Formula: see text]和 ε→0 的极限下,湍流雷诺数 εRλ 和板厚分别保持固定(分别为 O(1) 和 O(λ))。但是考虑了各种极限情况,以解释相关的过渡机制。有人认为,在过渡过程中可能有两种条纹状结构起作用:(i) 出现在下游区域并由上游流动中的流向涡度产生的结构;(ii) 集中在前缘附近并由上游流动中的板法线涡度产生的结构。前者不受前缘几何形状的影响,通常被称为克莱巴诺夫模式,而后者受前缘几何形状的强烈影响,并且在外观上更像是流向涡。