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Updated: May 9, 2026

Magnetically Induced Rotating Rayleigh-Taylor Instability
Published on: March 3, 2017
Logarithmic boundary layers in strong Taylor-Couette turbulence
Sander G Huisman1, Sven Scharnowski, Christian Cierpka
1Department of Applied Physics and J. M. Burgers Centre for Fluid Dynamics, University of Twente, P.O. Box 217, 7500 AE Enschede, The Netherlands.
This study measures turbulent Taylor-Couette flow properties, finding the von Kármán constant approaches 0.40 at high Taylor numbers (Ta). Velocity variance profiles show universal behavior, independent of friction velocity.
Area of Science:
- Fluid dynamics
- Turbulence research
- Experimental fluid mechanics
Background:
- Turbulent boundary layers are crucial in many engineering applications.
- Taylor-Couette flow provides a well-defined system to study turbulence.
- Understanding flow behavior near boundaries is essential for predicting drag and heat transfer.
Purpose of the Study:
- To experimentally investigate boundary layer properties in highly turbulent Taylor-Couette flow.
- To determine the von Kármán constant in this flow regime.
- To analyze the scaling and universality of velocity variance profiles.
Main Methods:
- Utilizing high-resolution particle image velocimetry (PIV).
- Employing particle tracking velocimetry (PTV) for detailed flow measurements.
- Conducting experiments in a turbulent Taylor-Couette flow setup up to Re=2×10^6 (Ta=6.2×10^12).
Main Results:
- The mean azimuthal velocity profile fits the von Kármán log law (u+=1/κ lny+ +B).
- The von Kármán constant (κ) approaches approximately 0.40 for large Taylor numbers (Ta).
- Velocity variance profiles exhibit universal peaks and collapse when rescaled by driving velocity, not friction velocity.
Conclusions:
- The von Kármán constant in turbulent Taylor-Couette flow is dependent on the driving strength (Ta).
- Logarithmic scaling of velocity variance is observed, similar to channel and pipe flows.
- Boundary layer behavior in this flow regime shows universal characteristics.
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