Resistive forces associated to boundary layers (‘friction’) are usually out of scale in physical models of hydraulic structures, especially in the case of hydraulically smooth walls, generating distortions in the model results known as scale effects, that can be problematic in some relevant engineering problems. These scale effects can be quantified and corrected using suitable numerical models. In this paper the accuracy of using numerical simulation through the Reynolds Averaged Navier-Stokes (RANS) approximation in order to represent the head losses introduced by friction in hydraulically smooth walls is evaluated for a wide range of Reynolds scales. This is performed by comparing the numerical results for fully developed flow on circula...
The purpose of this report is to investigate the phenomenon in hydraulic models known as scale effe...
To estimate friction introduced by plastering strips inside of laboratory tunnels, an equation named...
Rough-wall boundary layers become aerodynamically smooth if the ‘roughness Reynolds number’ Re*=u*z0...
A logarithmic velocity profile has been used, in conjunction with a formulation for the origin of th...
The presence of a wall significantly influences the turbulence structure of a flow. Wall effects are...
The sensitivity of a large range of turbulence closures to the near-wall grid resolution is assessed...
Physical hydraulic scale models are valuable tools for engineers to use when solving complex hydraul...
The present work is focused on the development of a modeling framework for scale-resolving simulatio...
The thesis describes the design, calibration and use of a floating element skin friction meter in sm...
One of the most important tasks of engineering hydraulics is to determine the energy loss during the...
The turbulent boundary layer is one of the most fundamental and important applications of fluid mech...
For centuries, scientists have been attempting to map complex hydraulic processes to empirical formu...
peer reviewedNumerical modelling is commonly used in a large range of environmental fluid mechanics ...
This paper reports some results of turbulent boundary layer computation. The calculation is made ass...
This article concerns the turbulent flow of Herschel–Bulkley slurries through circular horizontal pi...
The purpose of this report is to investigate the phenomenon in hydraulic models known as scale effe...
To estimate friction introduced by plastering strips inside of laboratory tunnels, an equation named...
Rough-wall boundary layers become aerodynamically smooth if the ‘roughness Reynolds number’ Re*=u*z0...
A logarithmic velocity profile has been used, in conjunction with a formulation for the origin of th...
The presence of a wall significantly influences the turbulence structure of a flow. Wall effects are...
The sensitivity of a large range of turbulence closures to the near-wall grid resolution is assessed...
Physical hydraulic scale models are valuable tools for engineers to use when solving complex hydraul...
The present work is focused on the development of a modeling framework for scale-resolving simulatio...
The thesis describes the design, calibration and use of a floating element skin friction meter in sm...
One of the most important tasks of engineering hydraulics is to determine the energy loss during the...
The turbulent boundary layer is one of the most fundamental and important applications of fluid mech...
For centuries, scientists have been attempting to map complex hydraulic processes to empirical formu...
peer reviewedNumerical modelling is commonly used in a large range of environmental fluid mechanics ...
This paper reports some results of turbulent boundary layer computation. The calculation is made ass...
This article concerns the turbulent flow of Herschel–Bulkley slurries through circular horizontal pi...
The purpose of this report is to investigate the phenomenon in hydraulic models known as scale effe...
To estimate friction introduced by plastering strips inside of laboratory tunnels, an equation named...
Rough-wall boundary layers become aerodynamically smooth if the ‘roughness Reynolds number’ Re*=u*z0...