The trajectory, penetration and mixing efficiency of lateral air jet injection into typical combustor flowfields in the absence of combustion were investigated so as to characterize the time-mean and turbulence flowfield for a variety of configurations and input parameters, recommend appropriate turbulence model advances, and implement and exhibit results of flowfield predictions. A combined experimental and theoretical approach was followed, in a modified version of the test facility, equipped initially with one and two lateral jets, located one test-section downstream of the inlet
Mean temperature profiles calculated with an interactive microcomputer code which evaluates dilution...
Experimental and computational results on the mixing of single, double, and opposed rows of jets wit...
An experimental investigation has been conducted of the isothermal mixing of a turbulent jet injecte...
Experiments have been conducted to document the time-mean and turbulent flowfield of a deflected tur...
Experiments have been conducted to obtain the time-mean and turbulent quantities of opposed lateral ...
Studies are concerned with experimental and theoretical research on 2-D axisymmetric geometries unde...
The 2-D axisymmetric geometries under low speed, nonreacting, turbulent, swirling flow conditions we...
The arrangement of multiple jets issuing perpendicularly to a crossflow is a fundamental fluid flow...
Combustor design phenomena; recirculating flows research; single-wire, six-orientation, eddy dissipa...
A computational effort was undertaken to analyze the details of fluid flow in Lean-Direct Injection ...
The design of a supersonic combustor which uses transverse jet injection into a supersonic flow (TJI...
A series of progressively finer grid systems to calculate the single jet in cross-flow experimentall...
Experiments were conducted to characterize the time-mean and turbulent flow field of a deflected tur...
Parametric tests were conducted to quantify the mixing of opposed rows of jets (two-sided injection)...
The combustor designer is typically required to design liner orifices that effectively mix air jets ...
Mean temperature profiles calculated with an interactive microcomputer code which evaluates dilution...
Experimental and computational results on the mixing of single, double, and opposed rows of jets wit...
An experimental investigation has been conducted of the isothermal mixing of a turbulent jet injecte...
Experiments have been conducted to document the time-mean and turbulent flowfield of a deflected tur...
Experiments have been conducted to obtain the time-mean and turbulent quantities of opposed lateral ...
Studies are concerned with experimental and theoretical research on 2-D axisymmetric geometries unde...
The 2-D axisymmetric geometries under low speed, nonreacting, turbulent, swirling flow conditions we...
The arrangement of multiple jets issuing perpendicularly to a crossflow is a fundamental fluid flow...
Combustor design phenomena; recirculating flows research; single-wire, six-orientation, eddy dissipa...
A computational effort was undertaken to analyze the details of fluid flow in Lean-Direct Injection ...
The design of a supersonic combustor which uses transverse jet injection into a supersonic flow (TJI...
A series of progressively finer grid systems to calculate the single jet in cross-flow experimentall...
Experiments were conducted to characterize the time-mean and turbulent flow field of a deflected tur...
Parametric tests were conducted to quantify the mixing of opposed rows of jets (two-sided injection)...
The combustor designer is typically required to design liner orifices that effectively mix air jets ...
Mean temperature profiles calculated with an interactive microcomputer code which evaluates dilution...
Experimental and computational results on the mixing of single, double, and opposed rows of jets wit...
An experimental investigation has been conducted of the isothermal mixing of a turbulent jet injecte...