Numerical simulations of the three-dimensional flow and heat transfer in a rectangular duct with a 180 C bend were performed. Results are presented for Reynolds numbers of 17,000 and 37,000 and for aspect ratios of 0.5 and I.O. A kappa-omega turbulence model with no reference to distance to a wall is used. Direct comparison between single block and multiblock grid calculations are made. Heat transfer and velocity distributions are compared to available literature with good agreement. The multi-block grid system is seen to produce more accurate results compared to a single-block grid with the same number of cells
In current and advanced gas turbine engines, increased speeds, pressures and temperatures are used t...
A computational study of three-dimensional turbulent flow and heat transfer was performed in four ty...
In this study, five models, including the standard k-epsilon (SKE), realizable k-epsilon (RKE), SST ...
Results from numerical simulations of air flow and heat transfer in a 'branched duct' geometry are p...
This study comprehensively simulate the use of k-ε model for predicting flow and heat transfer with ...
A complete set of benchmark quality data for the flow and heat transfer within a large rectangular t...
Due to the character of the original source materials and the nature of batch digitization, quality ...
It has been a common practice that serpentine cooling passages are used in gas turbine blade to enha...
Abstract. Results of numerical simulation of three-dimensional turbulent flow and endwall heat trans...
Numerical results are presented for flow in a rotating internal passage with a 180 degree turn and r...
This study investigated the Navier-Stokes computations of the surface heat transfer coefficients of ...
In order to achieve higher thermal efficiency and power output, the gas turbine inlet temperature of...
Local heat transfer rates and overall pressure losses were determined for serpentine passages of squ...
Purpose - The employment of continuous ribs in a passage involves a noticeable pressure drop penalty...
AbstractThe cooling system of gas turbine blades understanding and improvement is increasing desires...
In current and advanced gas turbine engines, increased speeds, pressures and temperatures are used t...
A computational study of three-dimensional turbulent flow and heat transfer was performed in four ty...
In this study, five models, including the standard k-epsilon (SKE), realizable k-epsilon (RKE), SST ...
Results from numerical simulations of air flow and heat transfer in a 'branched duct' geometry are p...
This study comprehensively simulate the use of k-ε model for predicting flow and heat transfer with ...
A complete set of benchmark quality data for the flow and heat transfer within a large rectangular t...
Due to the character of the original source materials and the nature of batch digitization, quality ...
It has been a common practice that serpentine cooling passages are used in gas turbine blade to enha...
Abstract. Results of numerical simulation of three-dimensional turbulent flow and endwall heat trans...
Numerical results are presented for flow in a rotating internal passage with a 180 degree turn and r...
This study investigated the Navier-Stokes computations of the surface heat transfer coefficients of ...
In order to achieve higher thermal efficiency and power output, the gas turbine inlet temperature of...
Local heat transfer rates and overall pressure losses were determined for serpentine passages of squ...
Purpose - The employment of continuous ribs in a passage involves a noticeable pressure drop penalty...
AbstractThe cooling system of gas turbine blades understanding and improvement is increasing desires...
In current and advanced gas turbine engines, increased speeds, pressures and temperatures are used t...
A computational study of three-dimensional turbulent flow and heat transfer was performed in four ty...
In this study, five models, including the standard k-epsilon (SKE), realizable k-epsilon (RKE), SST ...