Optimal Taylor-Couette turbulence
Dennis P. M. van Gils, Sander G. Huisman, Siegfried Grossmann, Chao, Sun, Detlef Lohse

TL;DR
This study investigates highly turbulent Taylor-Couette flow with independent cylinder rotation, revealing a universal flux exponent, optimal angular velocity ratio, and complex flow structures through experimental torque and velocity profile analysis.
Contribution
It provides the first comprehensive experimental analysis of angular velocity flux scaling, neutral line dynamics, and flow regimes in high Taylor number Taylor-Couette turbulence.
Findings
Effective flux exponent b3 b1 0.03 across all rotation ratios
Maximum angular velocity flux at a_opt b1 0.33, indicating optimal counter-rotation
Bimodal velocity distribution and inward neutral line for strong counter-rotation
Abstract
Strongly turbulent Taylor-Couette flow with independently rotating inner and outer cylinders with a radius ratio of \eta = 0.716 is experimentally studied. From global torque measurements, we analyse the dimensionless angular velocity flux Nu_\omega(Ta, a) as a function of the Taylor number Ta and the angular velocity ratio a = -\omega_o/\omega_i in the large-Taylor-number regime 10^{11} \lesssim Ta \lesssim 10^{13}. We analyse the data with the common power-law ansatz for the dimensionless angular velocity transport flux Nu_\omega(Ta, a) = f(a)Ta^\gamma, with an amplitude f(a) and an exponent \gamma. The data are consistent with one effective exponent \gamma = 0.39\pm0.03 for all a. The amplitude of the angular velocity flux f(a) = Nu_\omega(Ta, a)/Ta^0.39 is measured to be maximal at slight counter-rotation, namely at an angular velocity ratio of a_opt = 0.33\pm0.04. This value is…
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