Structure of Zero Pressure Gradient High Reynolds Number Turbulent Boundary Layers
Doktorsavhandling, 2008

This thesis presents part of the large research program funded by the European Commission called Wallturb: A European synergy for the assessment of wall turbulence. The main aim of this research program is to create new experimental and numerical databases on the characteristics of turbulent wall- bounded flows, especially turbulent boundary layers. The goal is that these databases will be used to gain more insight into the physical mechanisms governing the dynamics of these flows. This knowledge is deemed essential for the future development of efficient and physical turbulence modeling strategies, which are in turn crucial to aircraft and other industries for sustainable development, especially under the pressure of high oil prices and operational costs. The signature experiment of Wallturb was the multi-investigator, multi-system, multi-point investigation carried out in the 20m test section of the boundary layer research facility at LML Lille, France in 2006. This thesis is focused primarily on the part of that investigation which utilized the 143 probe hot-wire array belonging to the Turbulence Research Laboratory of Chalmers, and only on the two zero- pressure gradient boundary layer experiments at Reθ of 9800 and 19 100. A new hot-wire calibration method was developed and utilized for this investigation. The method is based on a polynomial curve fitting approximation which expresses the instantaneous velocity as a function of instantaneous voltage. The results showed that even a second order polynomial approximation yields very good agreement between the measured profiles (or computed profiles after the calibration) and the reference profiles used in the calibration. The method also provides an opportunity to do the calibration on the fly as long as the convergence of the high order voltage statistics can be satisfied. The large scale motions of the turbulence were studied in detail using two-dimensional two-point cross-correlations maps on different planes within the measurement domain. It was observed that the elongated correlations exist at every wall-normal position above the buffer layer. These elongated structures were relatively more significant in the log layer. The investigation using the proper orthogonal decomposition showed that the POD (in conjunction with Fourier analysis in the statistically homogeneous and stationary directions) can effectively represent the total kinetic energy with a small number of modes. At both Reynolds numbers, it was possible to recover almost 90% of the total turbulence kinetic energy within the entire boundary layer with only four POD modes. The reconstructed velocity fluctuations on the spanwise-wall-normal plane show how organized motions of turbulence with significant amounts of energy interact with each other across the boundary layer. It was also possible to observe the interaction between the inner and outer layers of turbulence using these reconstructed velocity fields.

Fourier decomposition.

proper orthogonal decomposition

large scale structures

Turbulent boundary layers

zero pressure gradient

wind tunnel




two-point correlations

high Reynolds number

HA2 Hörsalsvägen 4, Göteborg
Opponent: Professor Julio Soria, Department of Mechanical and Aerospace Engineering, Monash University, Australia


Murat Tutkun

Chalmers, Tillämpad mekanik, Strömningslära


Strömningsmekanik och akustik



Doktorsavhandlingar vid Chalmers tekniska högskola. Ny serie: 2847

HA2 Hörsalsvägen 4, Göteborg

Opponent: Professor Julio Soria, Department of Mechanical and Aerospace Engineering, Monash University, Australia

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