Results 21 to 30 of about 140,231 (211)

Logarithmic mean temperature profiles and their connection to plume emissions in turbulent Rayleigh-B\'enard convection [PDF]

open access: yes, 2015
Two-dimensional simulations of Rayleigh-B\'enard convection at $Ra = 5\times10^{10}$ show that vertical logarithmic mean temperature profiles can be observed in regions of the boundary layer where thermal plumes are emitted.
Grossmann, Siegfried   +4 more
core   +2 more sources

Entropy Fluctuations and Correlations in Compressible Turbulent Plane Channel Flow

open access: yesEntropy
The thermodynamic turbulence structure of compressible aerodynamic flows is often characterised by the correlation coefficient of entropy with pressure or temperature.
G. A. Gerolymos, I. Vallet
doaj   +1 more source

Direct Numerical Simulation of Supersonic Turbulent Boundary Layer with Spanwise Wall Oscillation

open access: yesEnergies, 2016
Direct numerical simulations (DNS) of Mach = 2.9 supersonic turbulent boundary layers with spanwise wall oscillation (SWO) are conducted to investigate the turbulent heat transport mechanism and its relation with the turbulent momentum transport.
Weidan Ni   +3 more
doaj   +1 more source

SYMMETRY CLASSIFICATION OF NEWTONIAN INCOMPRESSIBLEFLUID’S EQUATIONS FLOW IN TURBULENT BOUNDARY LAYERS [PDF]

open access: yesVestnik KRAUNC: Fiziko-Matematičeskie Nauki, 2017
Lie group method is applicable to both linear and non-linear partial differential equations, which leads to find new solutions for partial differential equations.
Nadjafikhah M., Hejazi S.R.
doaj   +1 more source

Higher-Order Correlations Between Thermodynamic Fluctuations in Compressible Aerodynamic Turbulence

open access: yesEntropy
This paper studies the exact and approximate relations between fluctuations in thermodynamic variables (pressure, density and temperature) that are imposed by the dilute-gas (Z=1) equation-of-state (EoS), which is a satisfactory approximation of air ...
Georges A. Gerolymos, Isabelle Vallet
doaj   +1 more source

Program for calculating laminar and turbulent boundary layers in arbitrary pressure gradients [PDF]

open access: yes, 1972
Computer program predicts growth of boundary layers along any surface where air is flowing. Two integral methods, Cohen-Reshotko and Sasman-Cresici, calculate laminar boundary layers and turbulent boundary layers, respectively; Schlichting-Granville ...
Mcnally, W. D.
core   +1 more source

A New TKE‐Based Parameterization of Atmospheric Turbulence in the Canadian Global and Regional Climate Models

open access: yesJournal of Advances in Modeling Earth Systems, 2019
A new semi‐empirical turbulence parameterization is presented. Key features of the scheme include representation of turbulent diffusivities in terms of the turbulent kinetic energy that is determined by solving a quasi‐equilibrium form of the equation ...
Y. He, N. A. McFarlane, A. H. Monahan
doaj   +1 more source

Properties of the turbulent/non-turbulent interface in boundary layers

open access: yes, 2016
The turbulent/non-turbulent interface is analysed in a direct numerical simulation of a boundary layer in the range $Re_\theta=2800-6600$, with emphasis on the behaviour of the relatively large-scale fractal intermittent region.
Borrell, Guillem, Jiménez, Javier
core   +1 more source

On Reflection of Shock Waves from Boundary Layers [PDF]

open access: yes, 1952
Measurements of the reflection characteristics of shock waves from a flat surface with a laminar and turbulent boundary layer are presented. The investigations were carried out at Mach numbers from about 1.3 to 1.5 and a Reynolds number of 0.9 x 10^4.
Dhawan, S., Liepmann, H. W., Roshko, A.
core   +1 more source

Bubbly Turbulent Drag Reduction Is a Boundary Layer Effect [PDF]

open access: yes, 2007
In turbulent Taylor-Couette flow, the injection of bubbles reduces the overall drag. On the other hand, rough walls enhance the overall drag. In this work, we inject bubbles into turbulent Taylor-Couette flow with rough walls (with a Reynolds number up ...
Berg, Thomas H. van den   +3 more
core   +2 more sources

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