[[abstract]]The flowfields of a side-dump combustor with various number of side-inlet guide-vane are measured using laser-Doppler velocimetry (LDV). The Reynolds number based on the bulk mean velocity and combustor diameter was 2.6 x 10(4). Quantities such as mean velocity, turbulence intensity, turbulent kinetic energy, vorticity, friction factor, and wall static pressure oscillation are used to characterize the fluid flow. In the dome region of the inlet-jet plane, there is one pair of counter-rotating vortices for the no-vane, one-vane, and two-vane cases and two pairs of counter-rotating vortices for the three-vane case, respectively. This trend is reversed in the impinging plane. The combustor flowfield downstream of the X-c(*) = 2.5 s...
The purpose of this research was to analyze the flow behavior of air through a combustor and pilot a...
Turbulence measurements are made in a novel gas tur- bine rig facility recently used to study combus...
The aim of this project is to investigate the secondary flow pattern downstream ofa low pressure tur...
[[abstract]]The axial and transverse mean velocity and turbulence intensity components as well as Re...
[[abstract]]The effects of impinging flow from side inlet to a dump combustor on the recirculating f...
Any outlet restriction downstream of pressure gain combustion (PGC), such as turbine blades, affects...
This paper reports an experimental investigation of the flow field inside a low aspect ratio dump co...
AbstractThis paper reports an experimental investigation of the flow field inside a low aspect ratio...
The combustor and turbine of a gas turbine engine are directly connected, and their flow fields and ...
[[abstract]]A study of turbulent mixing of two confined jets in a side-dump combustor was carried ou...
A detailed investigation into the aerodynamics of a modern gas turbine combustor is reported in this...
Simultaneous two-component laser-Doppler-velocimeter measurements were made in an axisymmetric sudde...
A model reactor is used to investigate the extent to which the overall performance and detailed flow...
As the research into the improvement of gas turbine performance progresses, the combustor- turbine i...
This study describes a rotating detonation combustor (RDC) equipped with a set of nozzle guide vanes...
The purpose of this research was to analyze the flow behavior of air through a combustor and pilot a...
Turbulence measurements are made in a novel gas tur- bine rig facility recently used to study combus...
The aim of this project is to investigate the secondary flow pattern downstream ofa low pressure tur...
[[abstract]]The axial and transverse mean velocity and turbulence intensity components as well as Re...
[[abstract]]The effects of impinging flow from side inlet to a dump combustor on the recirculating f...
Any outlet restriction downstream of pressure gain combustion (PGC), such as turbine blades, affects...
This paper reports an experimental investigation of the flow field inside a low aspect ratio dump co...
AbstractThis paper reports an experimental investigation of the flow field inside a low aspect ratio...
The combustor and turbine of a gas turbine engine are directly connected, and their flow fields and ...
[[abstract]]A study of turbulent mixing of two confined jets in a side-dump combustor was carried ou...
A detailed investigation into the aerodynamics of a modern gas turbine combustor is reported in this...
Simultaneous two-component laser-Doppler-velocimeter measurements were made in an axisymmetric sudde...
A model reactor is used to investigate the extent to which the overall performance and detailed flow...
As the research into the improvement of gas turbine performance progresses, the combustor- turbine i...
This study describes a rotating detonation combustor (RDC) equipped with a set of nozzle guide vanes...
The purpose of this research was to analyze the flow behavior of air through a combustor and pilot a...
Turbulence measurements are made in a novel gas tur- bine rig facility recently used to study combus...
The aim of this project is to investigate the secondary flow pattern downstream ofa low pressure tur...