In what follows we develop a possible interpretation of these results, based on the working hypothesis that a class of very-large-scale ‘structures’ with statistical

A first campaign was done based on a high magnification 2C2D PIV in the near wall region in order to capture the near wall scales and the mean gradient.. A second experiment of

2.. Now, as hypersonic flight becomes more important in today’s research, the community finds itself once again building on available knowledge to improve its understanding for

The results show that the turbulent boundary layer separation of wing can be obviously sup- pressed and the maximum lift coefficient is improved at high Reynolds number with

Along that direction, weakly correlated structures present a maximum length of O 18δ in channels, and O 7δ in boundary layers, attained at the outer and logarithmic

An explicit wall model based on a power-law velocity profile for the description of the turbulent boundary layer is proposed for high Reynolds number flow RANS simulations.. This

While most studies have focussed on channel flows and zero pressure gradient (ZPG) boundary layer flows, our understanding of wall turbulence under the influence of a

and Monson, D.J., “The Hypersonic Shock Wave- Turbulent Boundary Layer Interaction Generated by a Sharp Fin at Mach 8.2,” AIAA Paper No. and Shapey, B.L.,

turbulent boundary layer and a laminar free-stream, we identify a layer—near the junction between the log and wake layers of the turbulent boundary layer—where significant

of pairing noise like in jets at high Reynolds number : less noisy jets are indeed observed for a natural smooth development of their turbulent boundary layer. This is of course not

standard k–ω model near the wall to a high Reynolds number version of the k–ε model in the outer portion of the boundary layer.. „ Contains a modified turbulent viscosity

Jones, M.B., Marusic, I. and Perry, AE 2001 Evolution and structure of sink-flow turbulent boundary layers. and Kaltenbach, H.J. 2004 A priori and a posteriori tests of

increase of heat transfer coecient in the turbulent boundary layer at high particle Reynolds number, Re P > 100, is the same as for a stationary particle.. In these experiments

Chamberlain, Rachel P., "Articulations of Liberation and Agency in Yanagi Miwa's "Elevator Girls"." Thesis, Georgia State University,

Keywords: Turbulent boundary layer; Heat/Mass Transfer Analogy; Large-Eddy Simulation (LES); Elliptic Blending Reynolds Stress Model (EB-RSM); Turbulent heat transfer

where the boundary layers are still laminar before separation. The use of high Reynolds number models implies the turbulent boundary layers and strong mixing, which shifts the

the same friction coefficient as a turbulent boundary layer in air flowing at the same Reynolds number and a local Mach number 1.29 times the Hach number of the helium flow..

where the boundary layers are still laminar before separation. The use of high Reynolds number models implies the turbulent boundary layers and strong mixing, which shifts the