Add to ORKGA turbulence generating grid has been used to increase the level of free-stream turbulence inside a 1.5 stage axial compressor to values typical of an embedded stage in a multi-stage machine.Hot-wire measurements taken in the rotor-stator axial gap have been ensemble-averaged to determine periodic fluctuations in turbulence level and velocity. These results are compared to measurements made at low turbulence levels without the turbulence grid. Increasing levels of free-stream turbulence are shown to reduce the magnitude of periodic disturbances produced by viscous interaction between the inlet guide vane (IGV) and rotor blade wakes
The unsteady behavior of a tip leakage flow downstream of a simulated axial compressor rotor has bee...
A broad investigation of the unsteady flow phenomena which occur in an axial flow compressor is pre...
Turbulence evolution in the near wake of a VAWT blade at a constant Reynolds number of 80,000 and an...
A turbulence generating grid has been used to increase the level of free-stream turbulence inside a ...
The influence of free-stream turbulence on wake dispersion and boundary layer transition processes h...
Current methods for designing compressor blades in axial turbomachines assume that the flow through ...
Compressor and turbine sections of axial flow turbomachines are subject to periodically disturbed fl...
The unsteady mid-span aerodynamics of an outlet stator row in a 1.5-stage low-speed axial compresso...
This paper analyzes the structure of turbulence in a single stage, low-speed axial fan with inlet gu...
The objective of this project is to measure the flow within axial turbomachines and use the data to ...
Axial compressors are used in power generation and aircraft engines. In compressor design, three dim...
The effects of grid generated free-stream turbulence on compressor cascade performance was measured ...
Flat plate turbulent boundary layers disturbed by periodic moving wakes have been observed in an exp...
Experiments are performed in an advanced design 1&1/2 stage high-speed axial compressor to investiga...
Direct numerical simulation and wind tunnel experiments have been used to study the effects of free-...
The unsteady behavior of a tip leakage flow downstream of a simulated axial compressor rotor has bee...
A broad investigation of the unsteady flow phenomena which occur in an axial flow compressor is pre...
Turbulence evolution in the near wake of a VAWT blade at a constant Reynolds number of 80,000 and an...
A turbulence generating grid has been used to increase the level of free-stream turbulence inside a ...
The influence of free-stream turbulence on wake dispersion and boundary layer transition processes h...
Current methods for designing compressor blades in axial turbomachines assume that the flow through ...
Compressor and turbine sections of axial flow turbomachines are subject to periodically disturbed fl...
The unsteady mid-span aerodynamics of an outlet stator row in a 1.5-stage low-speed axial compresso...
This paper analyzes the structure of turbulence in a single stage, low-speed axial fan with inlet gu...
The objective of this project is to measure the flow within axial turbomachines and use the data to ...
Axial compressors are used in power generation and aircraft engines. In compressor design, three dim...
The effects of grid generated free-stream turbulence on compressor cascade performance was measured ...
Flat plate turbulent boundary layers disturbed by periodic moving wakes have been observed in an exp...
Experiments are performed in an advanced design 1&1/2 stage high-speed axial compressor to investiga...
Direct numerical simulation and wind tunnel experiments have been used to study the effects of free-...
The unsteady behavior of a tip leakage flow downstream of a simulated axial compressor rotor has bee...
A broad investigation of the unsteady flow phenomena which occur in an axial flow compressor is pre...
Turbulence evolution in the near wake of a VAWT blade at a constant Reynolds number of 80,000 and an...