The main objectives for the NASA Jet Mixing Phase 3 program were: extension of the data base on the mixing of single sided rows of jets in a confined cross flow to discrete slots, including streamlined, bluff, and angled injections; quantification of the effects of geometrical and flow parameters on penetration and mixing of multiple rows of jets into a confined flow; investigation of in-line, staggered, and dissimilar hole configurations; and development of empirical correlations for predicting temperature distributions for discrete slots and multiple rows of dilution holes
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 ...
An existing empirical model of the temperature field downstream of single and multiple rows of jets ...
The objectives of the program were: (1) to extend the data base on mixing of a single-sided row of j...
Parametric tests were conducted to quantify the mixing of opposed rows of jets (two-sided injection)...
The effect of jet to mainstream density ratio, flow area convergence as encounted in transition sect...
The velocity and temperature distributions predicted by a 3-D numerical model and experimental measu...
A microcomputer code which displays 3-D oblique and 2-D plots of the temperature distribution downst...
The mixing performance in a mixing section of a rich burn/quick mix/lean burn (RQL) combustor was ca...
The objectives and status of a project to investigate various aspects of the jet in a confined cross...
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...
Experimental results are given on the mixing of a single row of jets with an isothermal mainstream i...
Study was conducted to determine penetration and mixing characteristics of multiple jets of ambient ...
Revised computer program on feasibility of water injection-cooled diffuser for nuclear rocket engine...
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 ...
An existing empirical model of the temperature field downstream of single and multiple rows of jets ...
The objectives of the program were: (1) to extend the data base on mixing of a single-sided row of j...
Parametric tests were conducted to quantify the mixing of opposed rows of jets (two-sided injection)...
The effect of jet to mainstream density ratio, flow area convergence as encounted in transition sect...
The velocity and temperature distributions predicted by a 3-D numerical model and experimental measu...
A microcomputer code which displays 3-D oblique and 2-D plots of the temperature distribution downst...
The mixing performance in a mixing section of a rich burn/quick mix/lean burn (RQL) combustor was ca...
The objectives and status of a project to investigate various aspects of the jet in a confined cross...
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...
Experimental results are given on the mixing of a single row of jets with an isothermal mainstream i...
Study was conducted to determine penetration and mixing characteristics of multiple jets of ambient ...
Revised computer program on feasibility of water injection-cooled diffuser for nuclear rocket engine...
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 ...
An existing empirical model of the temperature field downstream of single and multiple rows of jets ...