Two dimensional, quasi three dimensional and three dimensional theories for the prediction of pure tone fan noise due to the interaction of inflow distortion with a subsonic annular blade row were studied with the aid of an unsteady three dimensional lifting surface theory. The effects of compact and noncompact source distributions on pure tone fan noise in an annular cascade were investigated. Numerical results show that the strip theory and quasi three-dimensional theory are reasonably adequate for fan noise prediction. The quasi three-dimensional method is more accurate for acoustic power and model structure prediction with an acoustic power estimation error of about plus or minus 2db
In the prediction theory for the broad band noise generated from a multi-blade fan, the wake was div...
To address growing concerns regarding community noise due to air traffic, noise regulations are beco...
The method of computing radiated noise from a ducted rotor due to inflow distortion and turbulence a...
Fan noise including its generation, radiation characteristics, and suppression by acoustic treatment...
An analytical study was made of some possible rotor alone noise sources of dipole, quadrapole and mo...
An amplitude probability density function analysis technique for quantifying the degree of fan noise...
Far-field noise measurements were taken for three different installations of essentially the same fa...
A method is presented for interim use in assessing the noise generated by fans and compressors in tu...
Uniform-flow annular-duct Green's functions are the essential elements of the classical acoustic ana...
A ground test stand was used to obtain acoustic data on a full scale prototype fan designed for quie...
The prediction of fan noise is an important part to the prediction of overall turbofan engine noise....
Results of recent NASA research to reduce aircraft turbofan noise are described. As the bypass ratio...
Qualitative and quantitative spectral analyses are presented that give the broadband-noise, discrete...
Turbofan noise directivity calculated for two directivity models was compared with experimental, bla...
The overall aero and acoutic design features of eight 6-foot-diameter, single stage fans tested in a...
In the prediction theory for the broad band noise generated from a multi-blade fan, the wake was div...
To address growing concerns regarding community noise due to air traffic, noise regulations are beco...
The method of computing radiated noise from a ducted rotor due to inflow distortion and turbulence a...
Fan noise including its generation, radiation characteristics, and suppression by acoustic treatment...
An analytical study was made of some possible rotor alone noise sources of dipole, quadrapole and mo...
An amplitude probability density function analysis technique for quantifying the degree of fan noise...
Far-field noise measurements were taken for three different installations of essentially the same fa...
A method is presented for interim use in assessing the noise generated by fans and compressors in tu...
Uniform-flow annular-duct Green's functions are the essential elements of the classical acoustic ana...
A ground test stand was used to obtain acoustic data on a full scale prototype fan designed for quie...
The prediction of fan noise is an important part to the prediction of overall turbofan engine noise....
Results of recent NASA research to reduce aircraft turbofan noise are described. As the bypass ratio...
Qualitative and quantitative spectral analyses are presented that give the broadband-noise, discrete...
Turbofan noise directivity calculated for two directivity models was compared with experimental, bla...
The overall aero and acoutic design features of eight 6-foot-diameter, single stage fans tested in a...
In the prediction theory for the broad band noise generated from a multi-blade fan, the wake was div...
To address growing concerns regarding community noise due to air traffic, noise regulations are beco...
The method of computing radiated noise from a ducted rotor due to inflow distortion and turbulence a...