实际表面上各向同性和各向异性粗糙度分量引起的湍流产生和耗散研究

IF 1.1 Q4 ENGINEERING, MECHANICAL Journal of the Global Power and Propulsion Society Pub Date : 2022-08-25 DOI:10.33737/jgpps/151658
J. Ahrens, Sebastian Kurth, K. Cengiz, Lars Wein, J. Seume
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引用次数: 0

摘要

粗糙度通常由在与表面相切的方向上定向为各向异性或各向同性的结构组成,或者由两个分量叠加而成。粗糙度元件之间的相互作用对流体机械损失产生显著影响。经济高效地维护空气动力学相关部件(如叶片)表面的功能需要对流量的影响进行定量预测,这可以通过雷诺平均纳维-斯托克斯模拟(RANS)实现。用于模拟对流动的影响的已建立的粗糙度参数是等效砂粒粗糙度ks。相比之下,本文采用直接数值模拟(DNS)和浸没边界法(IBM)对各向异性、各向同性和叠加表面上的通道流动进行研究,以研究空气动力学损失,例如,由于湍流的产生和耗散。模拟结果表明,等效砂粒粗糙度不能正确预测各向异性和叠加表面的流动损失,因为实际上,由于湍流产生和耗散的改变,相对于各向异性结构的“攻角”会改变湍流。流动阻力和该迎角之间的非线性关系是压力梯度局部变化的结果。
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Investigation of turbulence production and dissipation due to isotropic and anisotropic roughness components on real surfaces
Roughness generally consists of structures that are either oriented anisotropic in directions tangential to the surface or isotropic, or a superposition of both components. Interactions between the roughness elements exert a significant influence on the fluid mechanical losses. Cost-effective maintenance of the functionality of the surfaces of aerodynamically relevant components such as blades requires the quantitative prediction of the influence on the flow, which can be achieved through Reynolds-Averaged-Navier-Stokes Simulations (RANS). An established roughness parameter used to model the influence on the flow is the equivalent sand grain roughness ks. By contrast, the research presented here employs Direct Numerical Simulations (DNS) with Immersed Boundary Method (IBM) of channel flows over anisotropic, isotropic, and superimposed surfaces in order to investigate the aerodynamic losses, for example, due to turbulent production and dissipation. The simulation results show that the equivalent sand grain roughness does not correctly predict flow losses from anisotropic and superimposed surfaces, because in reality, the “angle of attack” with respect to the anisotropic structures changes the turbulence due to altered turbulent production and dissipation. A non-linear relationship between the flow resistance and this angle of attack is a result of local changes in pressure gradients.
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来源期刊
Journal of the Global Power and Propulsion Society
Journal of the Global Power and Propulsion Society Engineering-Industrial and Manufacturing Engineering
CiteScore
2.10
自引率
0.00%
发文量
21
审稿时长
8 weeks
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