Invariant scaling laws for plane Couette flow with wall-transpiration

Author:

Dokoza Toni1ORCID,Hennings de Lara Joao Vinicius1ORCID,Oberlack Martin1ORCID

Affiliation:

1. Chair of Fluid Dynamics, Technical University of Darmstadt , Otto-Berndt-Straße 2, Darmstadt 64287, Germany

Abstract

The effect of the wall-transpiration Reynolds number ReV0 on the large-scale rolls of the plane Couette flow with wall-transpiration is investigated using resolvent analysis. We observe streamwise-elongated large-scale rolls, moving closer to the suction wall and becoming narrower in the wall-normal and spanwise direction as well as shortened in the streamwise direction for growing ReV0 due to the decreasing characteristic length of the sheared region. Invariant scaling laws describing the growth of the amplification gain over various parameters and determining the optimal parameters yielding most amplification are found enhancing our understanding of the influence on the coherent structures, which can be used to predict their exact size. In a potential second step, this allows to manipulate and efficiently modify these flow characteristics increasing the functionality for various engineering applications as for mass, momentum and heat transfer, which is dominated by turbulent superstructures. For large enough wall-transpiration, the most amplified structures are oblique at optimal streamwise wavenumbers αmax≠0 growing linearly with ReV0. The optimal spanwise wavenumber βmax yielding most amplified structures shows a polynomial dependence of second order on ReV0. For a constant ratio of the wall-transpiration and streamwise Reynolds numbers γ=ReV0Re, the most amplified structures occur at optimal streamwise Reynolds numbers represented by Remax·γa=C. The amplification gain changes its trend from growing with Re2 to decreasing with Re−1.368 after Remax is reached. The resulting streamwise structures are identical for each set of Remax and γ within this invariant scaling law.

Funder

German Academic Scholarship Foundation

Publisher

AIP Publishing

Reference48 articles.

1. W. Pfenninger , “ Untersuchungen über Reibungsverminderungen an Tragflügeln: insbesondere mit Hilfe von Grenzschichtabsaugung,” Ph.D. thesis ( Swiss Federal Institute of Technology in Zuerich, 1946).

2. Umschlagbeginn und absaugung;Jahrb. Dtsch. Akad. Luftfahrtforsch.,1942

3. P. Chiarulli and J.Freeman, “ Stability of the boundary layer,” AAF Technical Report No. F-TR-1197-IA ( Air Material Command, Wright Patterson Air Force Base, 1948), Vol. 6.

4. On the stability of the asymptotic suction boundary-layer profile;J. Fluid Mech.,1965

5. Non-linear instability of the asymptotic suction velocity profile;Q. J. Mech. Appl. Math.,1975

同舟云学术

1.学者识别学者识别

2.学术分析学术分析

3.人才评估人才评估

"同舟云学术"是以全球学者为主线,采集、加工和组织学术论文而形成的新型学术文献查询和分析系统,可以对全球学者进行文献检索和人才价值评估。用户可以通过关注某些学科领域的顶尖人物而持续追踪该领域的学科进展和研究前沿。经过近期的数据扩容,当前同舟云学术共收录了国内外主流学术期刊6万余种,收集的期刊论文及会议论文总量共计约1.5亿篇,并以每天添加12000余篇中外论文的速度递增。我们也可以为用户提供个性化、定制化的学者数据。欢迎来电咨询!咨询电话:010-8811{复制后删除}0370

www.globalauthorid.com

TOP

Copyright © 2019-2024 北京同舟云网络信息技术有限公司
京公网安备11010802033243号  京ICP备18003416号-3