A rotating rake mode measurement system was designed to measure acoustic duct modes generated by a fan stage. After analysis of the measured data, the mode coefficient amplitudes and phases were quantified. Early studies using this system found that mode power levels computed from rotating rake measured data would agree with the far-field power levels. However, this agreement required that the sound from the noise sources within the duct propagated outward from the duct exit without reflection and previous studies suggested conditions could exist where significant reflections could occur. This paper shows that mounting a second rake to the rotating system, with an offset in both the axial and the azimuthal directions, measures the data nece...
The method of computing radiated noise from a ducted rotor due to inflow distortion and turbulence a...
A detailed theoretical study of the acoustic propagation of spinning modes in acoustically treated o...
Continued progress to reduce fan noise emission from high bypass ratio engine ducts in aircraft incr...
The Rotating Rake mode measurement system was designed to measure acoustic duct modes generated by a...
An experimental measurement system was developed and implemented by the NASA Glenn Research Center i...
A technique is presented for the analysis of measured data obtained from a rotating microphone rake ...
The rotating microphone measurement technique and data analysis procedures are documented which are ...
The NASA Glenn Research Center's Advanced Noise Control Fan (ANCF) was developed in the early 1990s ...
Extensive measurements of the spinning acoustic mode structure in the NASA 48 inch Active Noise Cont...
The NASA Broadband Aeroacoustic Stator Simulation code was used to compute the acoustic field for hi...
A suppression prediction program based on the method of modal analysis for spinning mode propagation...
This report describes a procedure for enhancing the use of the basic rotating microphone system so a...
Uniform-flow annular-duct Green's functions are the essential elements of the classical acoustic ana...
A continuously rotating rake with radial microphones was developed to measure the inlet and exhaust ...
The recent Boundary-Layer-Ingesting Inlet/Distortion Tolerant Fan wind tunnel experiment at NASA Gle...
The method of computing radiated noise from a ducted rotor due to inflow distortion and turbulence a...
A detailed theoretical study of the acoustic propagation of spinning modes in acoustically treated o...
Continued progress to reduce fan noise emission from high bypass ratio engine ducts in aircraft incr...
The Rotating Rake mode measurement system was designed to measure acoustic duct modes generated by a...
An experimental measurement system was developed and implemented by the NASA Glenn Research Center i...
A technique is presented for the analysis of measured data obtained from a rotating microphone rake ...
The rotating microphone measurement technique and data analysis procedures are documented which are ...
The NASA Glenn Research Center's Advanced Noise Control Fan (ANCF) was developed in the early 1990s ...
Extensive measurements of the spinning acoustic mode structure in the NASA 48 inch Active Noise Cont...
The NASA Broadband Aeroacoustic Stator Simulation code was used to compute the acoustic field for hi...
A suppression prediction program based on the method of modal analysis for spinning mode propagation...
This report describes a procedure for enhancing the use of the basic rotating microphone system so a...
Uniform-flow annular-duct Green's functions are the essential elements of the classical acoustic ana...
A continuously rotating rake with radial microphones was developed to measure the inlet and exhaust ...
The recent Boundary-Layer-Ingesting Inlet/Distortion Tolerant Fan wind tunnel experiment at NASA Gle...
The method of computing radiated noise from a ducted rotor due to inflow distortion and turbulence a...
A detailed theoretical study of the acoustic propagation of spinning modes in acoustically treated o...
Continued progress to reduce fan noise emission from high bypass ratio engine ducts in aircraft incr...