The available data describing the incompressible zero-pressure-gradient boundary layer
are reviewed in association with a range of studies which are either new or, to date, not very …

This experimental investigation deals with the influence of turbulence intensities Tuδ⩽ 13%
and a ratio of integral length scale Λ11 to boundary layer thickness δ99. 5 smaller than two …

Hot-wire microsensors for the purpose of measuring the instantaneous velocity gradient
close to a wall were designed and their characteristics were evaluated. The sensors were …

This paper describes the evolution of an incompressible turbulent boundary layer on the flat
wall of an 'S'-shaped wind tunnel test section under the influence of changing streamwise …

A nano-sized crossed thermal anemometer (X-NSTAP) was developed and validated for
measurements of two-components of velocity at high Reynolds numbers. The new sensor …

Single-point turbulence statistics are here reported for zero pressure-gradient boundary
layers at Reynolds numbers based on the momentum thickness in the range 2530< Reθ< …

There are many engineering applications at Reynolds numbers orders of magnitude higher
than existing turbulent boundary layer studies. Currently, the mechanisms for turbulent …

In this research, turbulence parameters such as turbulence intensity, Kolmogorov length
scale, dissipation rate and velocity profiles at a cross section of flow over a flat plate are …

In this research, turbulence parameters such as turbulence intensity, Kolmogorov length
scale, dissipation rate and velocity profiles at a cross section of flow over a flat plate are …