Add to ORKGDownstream stator contribution to interaction noise of single-stage axial flow compresso
Axial compressors have inherently unsteady flow fields because of relative motion between rotor and ...
Inlet guide vane spacing effects on compressor noise reduction in turbojet engine
The noise generated by inlet turbulence impinging on a subsonic axial flow fan was studied as a func...
Far field noise propagation of rotor-stator interaction in single stage axial flow research compress...
Noise elimination in inlet-guide-vane - rotor interaction of single stage axial flow compresso
Inlet-guide-vane configuration and relative blade velocity effects on noise reduction from axial flo...
A study of compressor noise is presented, based upon supersonic, part-speed operation of a high hub/...
Turbojet engine noise reduction by increasing intake system guide vane-rotor blade spacin
Experiments are performed in an advanced design 1&1/2 stage high-speed axial compressor to investiga...
The role of the interaction of rotor tip flow irregularities (vortices and velocity defects) with do...
Although it is known that the flow field in a turbomachine is unsteady, current design tools do not ...
Tip-clearance (TC) noise is significant in compressors and has garnered scholarly attention for the ...
Thesis (Sc. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1997....
Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 2008.Includes...
The noise source caused by the interaction of the rotor tip flow irregularities (vortices and veloci...
Axial compressors have inherently unsteady flow fields because of relative motion between rotor and ...
Inlet guide vane spacing effects on compressor noise reduction in turbojet engine
The noise generated by inlet turbulence impinging on a subsonic axial flow fan was studied as a func...
Far field noise propagation of rotor-stator interaction in single stage axial flow research compress...
Noise elimination in inlet-guide-vane - rotor interaction of single stage axial flow compresso
Inlet-guide-vane configuration and relative blade velocity effects on noise reduction from axial flo...
A study of compressor noise is presented, based upon supersonic, part-speed operation of a high hub/...
Turbojet engine noise reduction by increasing intake system guide vane-rotor blade spacin
Experiments are performed in an advanced design 1&1/2 stage high-speed axial compressor to investiga...
The role of the interaction of rotor tip flow irregularities (vortices and velocity defects) with do...
Although it is known that the flow field in a turbomachine is unsteady, current design tools do not ...
Tip-clearance (TC) noise is significant in compressors and has garnered scholarly attention for the ...
Thesis (Sc. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1997....
Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 2008.Includes...
The noise source caused by the interaction of the rotor tip flow irregularities (vortices and veloci...
Axial compressors have inherently unsteady flow fields because of relative motion between rotor and ...
Inlet guide vane spacing effects on compressor noise reduction in turbojet engine
The noise generated by inlet turbulence impinging on a subsonic axial flow fan was studied as a func...