Add to ORKGFar field noise propagation of rotor-stator interaction in single stage axial flow research compresso
This thesis is an investigation into the production and prediction of broadband noise in axial compr...
May 1955Thesis written jointly by both authors: Thesis (M.S.)--Massachusetts Institute of Technology...
Abstract An experimental investigation of the aerodynamic response of the rotor blading of a single ...
Noise elimination in inlet-guide-vane - rotor interaction of single stage axial flow compresso
Downstream stator contribution to interaction noise of single-stage axial flow compresso
A study of compressor noise is presented, based upon supersonic, part-speed operation of a high hub/...
Inlet-guide-vane configuration and relative blade velocity effects on noise reduction from axial flo...
Theoretical study of discrete frequency noise generated by turbocompressors and blade
A three-stage axial-flow compressor was developed for a continuous transonic wind tunnel. The rotor-...
The results of a theoretical and experimental study on the role of aerodynamically-induced fluctuati...
Turbojet engine noise reduction by increasing intake system guide vane-rotor blade spacin
The noise generated by inlet turbulence impinging on a subsonic axial flow fan was studied as a func...
Nacelle design for turbofan engine compressor noise suppression on Douglas DC-8 aircraf
Inlet guide vane spacing effects on compressor noise reduction in turbojet engine
The method of computing radiated noise from a ducted rotor due to inflow distortion and turbulence a...
This thesis is an investigation into the production and prediction of broadband noise in axial compr...
May 1955Thesis written jointly by both authors: Thesis (M.S.)--Massachusetts Institute of Technology...
Abstract An experimental investigation of the aerodynamic response of the rotor blading of a single ...
Noise elimination in inlet-guide-vane - rotor interaction of single stage axial flow compresso
Downstream stator contribution to interaction noise of single-stage axial flow compresso
A study of compressor noise is presented, based upon supersonic, part-speed operation of a high hub/...
Inlet-guide-vane configuration and relative blade velocity effects on noise reduction from axial flo...
Theoretical study of discrete frequency noise generated by turbocompressors and blade
A three-stage axial-flow compressor was developed for a continuous transonic wind tunnel. The rotor-...
The results of a theoretical and experimental study on the role of aerodynamically-induced fluctuati...
Turbojet engine noise reduction by increasing intake system guide vane-rotor blade spacin
The noise generated by inlet turbulence impinging on a subsonic axial flow fan was studied as a func...
Nacelle design for turbofan engine compressor noise suppression on Douglas DC-8 aircraf
Inlet guide vane spacing effects on compressor noise reduction in turbojet engine
The method of computing radiated noise from a ducted rotor due to inflow distortion and turbulence a...
This thesis is an investigation into the production and prediction of broadband noise in axial compr...
May 1955Thesis written jointly by both authors: Thesis (M.S.)--Massachusetts Institute of Technology...
Abstract An experimental investigation of the aerodynamic response of the rotor blading of a single ...