The effect of jet to mainstream density ratio, flow area convergence as encounted in transition sections, and nonuniform mainstream profile upstream of dilution orifices on the mixing of a row of jets with a confined cross flow was quantified. It is found that: (1) jet spreading rate in transverse direction is increased with increasing J, H/D and with decreasing S/D; (2) the density ratio has only a second order effect on the jet mixing characteristics for a constant momentum ratio; (3) the temperature distributions in the jet mixing region are strongly influenced by the undisturbed mainstream profile; (4) flow area convergence enhances mixing in radial and transverse directions. An asymmetric convergent duct with flat wall injection has th...
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...
An experimental investigation has been carried out into the mixing of a row of jets injected into a ...
Parametric tests were conducted to quantify the mixing of opposed rows of jets (two-sided injection)...
A microcomputer code which displays 3-D oblique and 2-D plots of the temperature distribution downst...
Experimental results are given on the mixing of a single row of jets with an isothermal mainstream i...
The main objectives for the NASA Jet Mixing Phase 3 program were: extension of the data base on the ...
The velocity and temperature distributions predicted by a 3-D numerical model and experimental measu...
The objectives and status of a project to investigate various aspects of the jet in a confined cross...
An existing empirical model of the temperature field downstream of single and multiple rows of jets ...
Experimental and computational results on the mixing of single, double, and opposed rows of jets wit...
Test data is presented which allows determination of jet penetration and mixing of multiple cold air...
An experimental investigation of the mixing of nonreacting opposed rows of jets injected normal to a...
The mixing performance in a mixing section of a rich burn/quick mix/lean burn (RQL) combustor was ca...
An experimental investigation of the effects of jet inlet flow conditions has been conducted for the...
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...
An experimental investigation has been carried out into the mixing of a row of jets injected into a ...
Parametric tests were conducted to quantify the mixing of opposed rows of jets (two-sided injection)...
A microcomputer code which displays 3-D oblique and 2-D plots of the temperature distribution downst...
Experimental results are given on the mixing of a single row of jets with an isothermal mainstream i...
The main objectives for the NASA Jet Mixing Phase 3 program were: extension of the data base on the ...
The velocity and temperature distributions predicted by a 3-D numerical model and experimental measu...
The objectives and status of a project to investigate various aspects of the jet in a confined cross...
An existing empirical model of the temperature field downstream of single and multiple rows of jets ...
Experimental and computational results on the mixing of single, double, and opposed rows of jets wit...
Test data is presented which allows determination of jet penetration and mixing of multiple cold air...
An experimental investigation of the mixing of nonreacting opposed rows of jets injected normal to a...
The mixing performance in a mixing section of a rich burn/quick mix/lean burn (RQL) combustor was ca...
An experimental investigation of the effects of jet inlet flow conditions has been conducted for the...
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...
An experimental investigation has been carried out into the mixing of a row of jets injected into a ...