Add to ORKGThe NASA Glenn Research Center's Advanced Noise Control Fan (ANCF) was developed in the early 1990s to provide a convenient test bed to measure and understand fan-generated acoustics, duct propagation, and radiation to the farfield. A series of tests were performed primarily for the use of code validation and tool validation. Rotating Rake mode measurements were acquired for parametric sets of: (i) mode blockage, (ii) liner insertion loss, (iii) short ducts, and (iv) mode reflection
This report describes work by consultants to Diversitech Inc. for the NASA Glenn Research Center (GR...
In February 2017, aerodynamic and acoustic testing was completed on a scale-model high bypass ratio ...
This final report has been prepared by Honeywell Aerospace, Phoenix, Arizona, a unit of Honeywell In...
The NASA Glenn Research Center's Advanced Noise Control Fan (ANCF) was developed in the early 1990s ...
The 9- by 15-Foot Low Speed Wind Tunnel has been used for acoustic testing for more than 40 years. T...
The ANCF test bed is used for evaluating fan noise reduction concepts, developing noise measurement ...
In this paper, the results of an extensive assessment exercise carried out to establish the current ...
Extensive measurements of the spinning acoustic mode structure in the NASA 48 inch Active Noise Cont...
The Advanced Noise Control Fan (ANCF) (formerly the Active Noise Control Fan) was utilized in the de...
An Ultrasonic Configurable Fan Artificial Noise Source (UCFANS) was designed, built, and tested in s...
An experimental measurement system was developed and implemented by the NASA Glenn Research Center i...
The Rotating Rake mode measurement system was designed to measure acoustic duct modes generated by a...
An Ultrasonic Configurable Fan Artificial Noise Source (UCFANS) was designed, built, and tested in s...
The Advanced Noise Control Fan (ne Active Noise Control Fan - ANCF) was utilized in the design, test...
A Williams International FJ44-3A 3000-lb thrust class turbofan engine was tested in the NASA Glenn R...
This report describes work by consultants to Diversitech Inc. for the NASA Glenn Research Center (GR...
In February 2017, aerodynamic and acoustic testing was completed on a scale-model high bypass ratio ...
This final report has been prepared by Honeywell Aerospace, Phoenix, Arizona, a unit of Honeywell In...
The NASA Glenn Research Center's Advanced Noise Control Fan (ANCF) was developed in the early 1990s ...
The 9- by 15-Foot Low Speed Wind Tunnel has been used for acoustic testing for more than 40 years. T...
The ANCF test bed is used for evaluating fan noise reduction concepts, developing noise measurement ...
In this paper, the results of an extensive assessment exercise carried out to establish the current ...
Extensive measurements of the spinning acoustic mode structure in the NASA 48 inch Active Noise Cont...
The Advanced Noise Control Fan (ANCF) (formerly the Active Noise Control Fan) was utilized in the de...
An Ultrasonic Configurable Fan Artificial Noise Source (UCFANS) was designed, built, and tested in s...
An experimental measurement system was developed and implemented by the NASA Glenn Research Center i...
The Rotating Rake mode measurement system was designed to measure acoustic duct modes generated by a...
An Ultrasonic Configurable Fan Artificial Noise Source (UCFANS) was designed, built, and tested in s...
The Advanced Noise Control Fan (ne Active Noise Control Fan - ANCF) was utilized in the design, test...
A Williams International FJ44-3A 3000-lb thrust class turbofan engine was tested in the NASA Glenn R...
This report describes work by consultants to Diversitech Inc. for the NASA Glenn Research Center (GR...
In February 2017, aerodynamic and acoustic testing was completed on a scale-model high bypass ratio ...
This final report has been prepared by Honeywell Aerospace, Phoenix, Arizona, a unit of Honeywell In...