A theoretical model for the generation of blade-passage noise caused by the interaction of rotor wakes with the downstream stator blades in a fan stage has been compiled. This model has combined a description of the rotor wake based on existing experimental correlations with an existing theory for the response of the stator blades to those wakes. This model of the interaction-caused blade-passage noise has been used to examine some effects of blade geometry and flow conditions on the noise generated. A set of significant parameters has been identified to reduce this interaction-caused blade-passage frequency noise. A redesign of an existing fan with the use of these concepts has produced a theoretical noise reduction of more than 7 decibels
An analytical study was made of some possible rotor alone noise sources of dipole, quadrapole and mo...
Hand calculation procedures for predicting aerodynamic noise from propellers, rotors, and lift fan
Numerical simulations are used to investigate the noise generated by the passage of a rotor blade pa...
As turbofan engine designs move towards bypass ratios \u3e12 and corresponding low pressure ratios, ...
An existing fan stage was redesigned to reduce stator lift fluctuations and was acoustically tested ...
Results of recent NASA research to reduce aircraft turbofan noise are described. As the bypass ratio...
A combined analytical/computational approach for controlling of the noise generated by wake/blade-ro...
AbstractThe experimental investigation of leaned bypass stator vanes impact on the fan model acousti...
The noise source caused by the interaction of the rotor tip flow irregularities (vortices and veloci...
The role of the interaction of rotor tip flow irregularities (vortices and velocity defects) with do...
Advanced counter-rotation propellers have been indicated as possibly generating an unacceptable amou...
The noise generated by inlet turbulence impinging on a subsonic axial flow fan was studied as a func...
Fan noise including its generation, radiation characteristics, and suppression by acoustic treatment...
This paper presents results derived from a study investigating the rotor wake-OGV interaction source...
An aeroacoustic investigation was performed to assess the effects of adding mass flow at the trailin...
An analytical study was made of some possible rotor alone noise sources of dipole, quadrapole and mo...
Hand calculation procedures for predicting aerodynamic noise from propellers, rotors, and lift fan
Numerical simulations are used to investigate the noise generated by the passage of a rotor blade pa...
As turbofan engine designs move towards bypass ratios \u3e12 and corresponding low pressure ratios, ...
An existing fan stage was redesigned to reduce stator lift fluctuations and was acoustically tested ...
Results of recent NASA research to reduce aircraft turbofan noise are described. As the bypass ratio...
A combined analytical/computational approach for controlling of the noise generated by wake/blade-ro...
AbstractThe experimental investigation of leaned bypass stator vanes impact on the fan model acousti...
The noise source caused by the interaction of the rotor tip flow irregularities (vortices and veloci...
The role of the interaction of rotor tip flow irregularities (vortices and velocity defects) with do...
Advanced counter-rotation propellers have been indicated as possibly generating an unacceptable amou...
The noise generated by inlet turbulence impinging on a subsonic axial flow fan was studied as a func...
Fan noise including its generation, radiation characteristics, and suppression by acoustic treatment...
This paper presents results derived from a study investigating the rotor wake-OGV interaction source...
An aeroacoustic investigation was performed to assess the effects of adding mass flow at the trailin...
An analytical study was made of some possible rotor alone noise sources of dipole, quadrapole and mo...
Hand calculation procedures for predicting aerodynamic noise from propellers, rotors, and lift fan
Numerical simulations are used to investigate the noise generated by the passage of a rotor blade pa...