The present work aims to numerically investigate the effect of varying turning angle, ø = 30° - 180° on the performance of 3D turning diffuser and to develop the performance correlations via integrating the turning angle using Asymptotic Computational Fluid Dynamics (ACFD) technique. Among all the turbulence models examined, the best validated results were obtained with the Reynold Stress Model with enhanced wall treatment of =1.0 was applied for the intensive simulation. As the turning angle increased from 30˚ to 180˚, the pressure recovery was reduced by 89.3% and the flow uniformity index was raised by 27.7%. Minimal flow separation took place at 0.75 of 90˚ turning diffuser whereas maximum flow separation happened at 0.44&nbs...
Abstract: The present study involves the CFD analysis for the prediction of swirl effect on the char...
Numerical study was conducted on the effect a variation of flange angle on diffuser DAWT performance...
Curved diffusers are an integral component of the gas turbine engines of high-speed aircraft. These ...
The present work aims to numerically investigate the effect of varying turning angle, ø = 30° - 18...
The performance of turning diffuser regardless of its expansion type, i.e., two-dimensional (2-D) or...
The performances of turning diffuser are highly affected due to the nature of its geometries by the ...
It is often necessary in fluid flow systems to simultaneously decelerate and turn the flow. This can...
Despite the widespread use of diffusers in various industries, there is no comprehensive research so...
In this study, a new turning rapid diffuser has been developed using CFD analyses. Typically the di...
This thesis deals with modeling and simulation of an asymmetric plane diffuser which is the most int...
This research paper compared three k-ε family turbulence models; Standard k-ε, RNG k-ε and Realizabl...
In this thesis diffuser performance will be simulated with computational fluid dynamics, which will ...
In the present investigation the distribution of mean velocity, static pressure and total pressure a...
The primary goal of the project was to gain insight into the flow pattern in a mixed flow pump diffu...
This study presents numerical investigation on the performance of S-shaped air intake normal and agg...
Abstract: The present study involves the CFD analysis for the prediction of swirl effect on the char...
Numerical study was conducted on the effect a variation of flange angle on diffuser DAWT performance...
Curved diffusers are an integral component of the gas turbine engines of high-speed aircraft. These ...
The present work aims to numerically investigate the effect of varying turning angle, ø = 30° - 18...
The performance of turning diffuser regardless of its expansion type, i.e., two-dimensional (2-D) or...
The performances of turning diffuser are highly affected due to the nature of its geometries by the ...
It is often necessary in fluid flow systems to simultaneously decelerate and turn the flow. This can...
Despite the widespread use of diffusers in various industries, there is no comprehensive research so...
In this study, a new turning rapid diffuser has been developed using CFD analyses. Typically the di...
This thesis deals with modeling and simulation of an asymmetric plane diffuser which is the most int...
This research paper compared three k-ε family turbulence models; Standard k-ε, RNG k-ε and Realizabl...
In this thesis diffuser performance will be simulated with computational fluid dynamics, which will ...
In the present investigation the distribution of mean velocity, static pressure and total pressure a...
The primary goal of the project was to gain insight into the flow pattern in a mixed flow pump diffu...
This study presents numerical investigation on the performance of S-shaped air intake normal and agg...
Abstract: The present study involves the CFD analysis for the prediction of swirl effect on the char...
Numerical study was conducted on the effect a variation of flange angle on diffuser DAWT performance...
Curved diffusers are an integral component of the gas turbine engines of high-speed aircraft. These ...