Add to ORKGIn this paper, numerical predictions of acoustic transmission through a 3D stator obtained using the NASA BASS code are compared with experimentally measured data. The influence of vane count and stagger as well as frequency and mode order on the transmission loss is investigated. The data-theory comparisons indicate that BASS can predict all the important trends observed in the experimental data
This report describes work performed on Contract NAS3-27720AoI 13 as part of the NASA Advanced Subso...
The use of computational techniques in the area of acoustics is known as computational aeroacoustics...
AIAA Aviation 2020 Forum in Reno (USA) has been transformed in a International Virtual Event at the ...
In this paper, numerical predictions of acoustic transmission through a 3D stator obtained using the...
The BASS computational aeroacoustic code solves the fully nonlinear Euler equations in the time doma...
The BASS computational aeroacoustic code solves the fully nonlinear Euler equations in the time doma...
For high-speed ducted fans, when the rotor flowfield is shock-free, the main contribution to the inl...
The ability to predict fan noise within complex three-dimensional aircraft engine nacelle geometries...
A Navier-Stokes computer code is used to predict one of the ducted-fan engine acoustic modes that re...
AbstractIn this work, the NASA Glenn Research Center Broadband Aeroacoustic Stator Simulation (BASS)...
AbstractIn this work, the NASA Glenn Research Center Broadband Aeroacoustic Stator Simulation (BASS)...
The field of computational aeroacoustics (CAA) encompasses numerical techniques for calculating all ...
In this work, the NASA Glenn Research Center Broadband Aeroacoustic Stator Simulation (BASS) code is...
The application of the two-dimensional aeroacoustic blade row model of Smith [1] to stators of axial...
Two dimensional, quasi three dimensional and three dimensional theories for the prediction of pure t...
This report describes work performed on Contract NAS3-27720AoI 13 as part of the NASA Advanced Subso...
The use of computational techniques in the area of acoustics is known as computational aeroacoustics...
AIAA Aviation 2020 Forum in Reno (USA) has been transformed in a International Virtual Event at the ...
In this paper, numerical predictions of acoustic transmission through a 3D stator obtained using the...
The BASS computational aeroacoustic code solves the fully nonlinear Euler equations in the time doma...
The BASS computational aeroacoustic code solves the fully nonlinear Euler equations in the time doma...
For high-speed ducted fans, when the rotor flowfield is shock-free, the main contribution to the inl...
The ability to predict fan noise within complex three-dimensional aircraft engine nacelle geometries...
A Navier-Stokes computer code is used to predict one of the ducted-fan engine acoustic modes that re...
AbstractIn this work, the NASA Glenn Research Center Broadband Aeroacoustic Stator Simulation (BASS)...
AbstractIn this work, the NASA Glenn Research Center Broadband Aeroacoustic Stator Simulation (BASS)...
The field of computational aeroacoustics (CAA) encompasses numerical techniques for calculating all ...
In this work, the NASA Glenn Research Center Broadband Aeroacoustic Stator Simulation (BASS) code is...
The application of the two-dimensional aeroacoustic blade row model of Smith [1] to stators of axial...
Two dimensional, quasi three dimensional and three dimensional theories for the prediction of pure t...
This report describes work performed on Contract NAS3-27720AoI 13 as part of the NASA Advanced Subso...
The use of computational techniques in the area of acoustics is known as computational aeroacoustics...
AIAA Aviation 2020 Forum in Reno (USA) has been transformed in a International Virtual Event at the ...