Experimental and numerical investigations were performed in order to develop a technique of active flow control by aspiration applied to an annular axial compressor cascade. Continuous aspiration is applied through shaped slots located on the suction side of the blades and close to the suction side on the hub. Test cases with aspiration are compared to test cases with less or without aspiration to identify the influence of the aspiration. Additional measurements were done on a second annular cascade with reduced blade number, hence higher loading. This allowed investigating if the aspiration devices could compensate the increased losses that occur at higher loading. A simple model is introduced to predict the static pressure rise due to the...
Thesis (Ph.D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1999.I...
The tip clearance flow within industrial axial compressor rows has a significant impact on compresso...
The tip clearance flow of industrial axial compressor rotors has a significant impact on compressor ...
Both experiments and computations are performed and analyzed to investigate the effectiveness and me...
Aspiration in an axial compressor is normally regarded as sucking out the low momentum boundary laye...
At the Institute of Aeronautics and Astronautics of the Technische Universiẗat Berlin, an annular ca...
This paper describes the method to improve the stall margin of transonic axial flow compressor by co...
Abstract Blades tip leakage flow structure in axial compressors has dominant effects on flow stabili...
An analytical and experimental study of the performance changes and flow effects of rotor tip cleara...
This paper presents an experimental investigation of effects of axially non-uniform tip clearances o...
An experimental and analytical investigation was undertaken to determine the influence of asymmetric...
ABSTRACT The results of an experimental investigation of the flow in a high-speed annular compressor...
Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2001....
The effects of positively bowed blade on the aerodynamic performance of annular compressor cascades ...
This paper details an experimental investigation, using a linear cascade, into the effects of real g...
Thesis (Ph.D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1999.I...
The tip clearance flow within industrial axial compressor rows has a significant impact on compresso...
The tip clearance flow of industrial axial compressor rotors has a significant impact on compressor ...
Both experiments and computations are performed and analyzed to investigate the effectiveness and me...
Aspiration in an axial compressor is normally regarded as sucking out the low momentum boundary laye...
At the Institute of Aeronautics and Astronautics of the Technische Universiẗat Berlin, an annular ca...
This paper describes the method to improve the stall margin of transonic axial flow compressor by co...
Abstract Blades tip leakage flow structure in axial compressors has dominant effects on flow stabili...
An analytical and experimental study of the performance changes and flow effects of rotor tip cleara...
This paper presents an experimental investigation of effects of axially non-uniform tip clearances o...
An experimental and analytical investigation was undertaken to determine the influence of asymmetric...
ABSTRACT The results of an experimental investigation of the flow in a high-speed annular compressor...
Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2001....
The effects of positively bowed blade on the aerodynamic performance of annular compressor cascades ...
This paper details an experimental investigation, using a linear cascade, into the effects of real g...
Thesis (Ph.D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1999.I...
The tip clearance flow within industrial axial compressor rows has a significant impact on compresso...
The tip clearance flow of industrial axial compressor rotors has a significant impact on compressor ...