AbstractThe objective of present work was to develop a three-dimensional numerical simulation on the basis of the finite volume method for predicting the penetration and mixing characteristics of a single row of coolant jets injected normally into a heated crossflow in a constant area duct. Two types of mesh size were developed to evaluate the ability of the standard and the (RNG)k–ε turbulence models. The effects of jet-to-mainstream momentum flux ratio, in the range of 6.0–23.5 and duct height to hole diameter ratio and relative spacing of adjacent jets to hole diameter ratio, within the range of 4.0–12.0 and 2.0–4.0, respectively, were investigated. Comparisons between the present numerical results on the temperature profiles and the exp...
A microcomputer code which displays 3-D oblique and 2-D plots of the temperature distribution downst...
The objective of this study was to numerically investigate the mixing characteristics of two and thr...
To examine the mixing characteristics of circular jets in an axisymmetric can geometry, temperature ...
AbstractThe objective of present work was to develop a three-dimensional numerical simulation on the...
The mixing characteristics of coolant air jets with the hot gas exiting the gas turbine combustor’s ...
Mean temperature profiles calculated with an interactive microcomputer code which evaluates dilution...
This paper compares temperature field measurements from selected experiments on a single row, and op...
Experimental and computational results on the mixing of single, double, and opposed rows of jets wit...
This paper summarizes experimental and computational results on the mixing of opposed rows of jets w...
An experimental investigation has been carried out into the mixing of a row of jets injected into a ...
This paper addresses the mixing of air jets into the hot, fuel-rich products of a gas turbine primar...
This is the data of a direct simulation of a hot jet in cold channel crossflow. Three thermal bounda...
The mixing performance in a mixing section of a rich burn/quick mix/lean burn (RQL) combustor was ca...
The injection of fully-developed turbulent heated air from a tube into a cooler turbulent duct flow ...
Three dimensional mixing length models of a flow field immediately downstream of coolant injection t...
A microcomputer code which displays 3-D oblique and 2-D plots of the temperature distribution downst...
The objective of this study was to numerically investigate the mixing characteristics of two and thr...
To examine the mixing characteristics of circular jets in an axisymmetric can geometry, temperature ...
AbstractThe objective of present work was to develop a three-dimensional numerical simulation on the...
The mixing characteristics of coolant air jets with the hot gas exiting the gas turbine combustor’s ...
Mean temperature profiles calculated with an interactive microcomputer code which evaluates dilution...
This paper compares temperature field measurements from selected experiments on a single row, and op...
Experimental and computational results on the mixing of single, double, and opposed rows of jets wit...
This paper summarizes experimental and computational results on the mixing of opposed rows of jets w...
An experimental investigation has been carried out into the mixing of a row of jets injected into a ...
This paper addresses the mixing of air jets into the hot, fuel-rich products of a gas turbine primar...
This is the data of a direct simulation of a hot jet in cold channel crossflow. Three thermal bounda...
The mixing performance in a mixing section of a rich burn/quick mix/lean burn (RQL) combustor was ca...
The injection of fully-developed turbulent heated air from a tube into a cooler turbulent duct flow ...
Three dimensional mixing length models of a flow field immediately downstream of coolant injection t...
A microcomputer code which displays 3-D oblique and 2-D plots of the temperature distribution downst...
The objective of this study was to numerically investigate the mixing characteristics of two and thr...
To examine the mixing characteristics of circular jets in an axisymmetric can geometry, temperature ...