Simultaneous two-component laser-Doppler-velocimeter measurements were made in an axisymmetric sudden expansion to measure the flow properties of a confined, isothermal flowfield of a research dump combustor. Measurements of mean velocities, Reynolds stresses, and triple products were carried out at axial distances ranging from 0.38H (H = step height) to 18H downstream of the dump plane. Detailed experimental data are provided to help in understanding the behavior of turbulent transport characteristics of the confined shear layer. Data from this study could be used to upgrade or evaluate advanced numerical codes used to predict complex turbulent flows. The turbulent kinetic energy terms (i.e. convection, diffusion, and production terms) wer...
Simultaneous two component velocity measurements are acquired in a model, complex flow swirl stabili...
This paper describes two-dimensional back-scatter laser-Doppler anemometer mesurements in confined i...
Among the most challenging aspects of modern gas turbine engine design, particularly with aviation a...
The flow characteristics downstream of an axisymmetric sudden expansion is of basic importance to de...
[[abstract]]The axial and transverse mean velocity and turbulence intensity components as well as Re...
Simultaneous two-component laser velocimeter measurements were made in the turbulent flow field foll...
[[abstract]]The flowfields of a side-dump combustor with various number of side-inlet guide-vane are...
Laser Doppler velocimetry (LDV) measurement and large eddy simulation (LES) were used to study confi...
This paper reports an experimental investigation of the flow field inside a low aspect ratio dump co...
The current demands for high performance gas turbine engines can be reached by raising combustion te...
AbstractThis paper reports an experimental investigation of the flow field inside a low aspect ratio...
An experimental and computational study is reported for the flow of a turbulent jet discharging into...
Significant progress has been made in computational fluid dynamic (CFD) modeling of gas turbine syst...
An experimental and computational study is reported for the flow of a turbulent jet discharging into...
Measured values of three components of mean velocity and the six components of the ' turbulent ...
Simultaneous two component velocity measurements are acquired in a model, complex flow swirl stabili...
This paper describes two-dimensional back-scatter laser-Doppler anemometer mesurements in confined i...
Among the most challenging aspects of modern gas turbine engine design, particularly with aviation a...
The flow characteristics downstream of an axisymmetric sudden expansion is of basic importance to de...
[[abstract]]The axial and transverse mean velocity and turbulence intensity components as well as Re...
Simultaneous two-component laser velocimeter measurements were made in the turbulent flow field foll...
[[abstract]]The flowfields of a side-dump combustor with various number of side-inlet guide-vane are...
Laser Doppler velocimetry (LDV) measurement and large eddy simulation (LES) were used to study confi...
This paper reports an experimental investigation of the flow field inside a low aspect ratio dump co...
The current demands for high performance gas turbine engines can be reached by raising combustion te...
AbstractThis paper reports an experimental investigation of the flow field inside a low aspect ratio...
An experimental and computational study is reported for the flow of a turbulent jet discharging into...
Significant progress has been made in computational fluid dynamic (CFD) modeling of gas turbine syst...
An experimental and computational study is reported for the flow of a turbulent jet discharging into...
Measured values of three components of mean velocity and the six components of the ' turbulent ...
Simultaneous two component velocity measurements are acquired in a model, complex flow swirl stabili...
This paper describes two-dimensional back-scatter laser-Doppler anemometer mesurements in confined i...
Among the most challenging aspects of modern gas turbine engine design, particularly with aviation a...