A set of long chord stator vanes was designed to replace the vanes in an existing fan stage. The long chord stator vanes consisted of a turning section and axial extension pieces, all of which incorporated acoustic damping material. The long chord stator vanes were tested in two lengths, with the long version giving more noise reduction than the short, primarily because of the additional lining material. The noise reduction achieved with the acoustically treated long chord stator vanes was compared with the reduction achieved by an acoustically treated exhaust splitter. The long chord stator was at least as good as the splitter as a method for incorporating acoustic lining material. In addition, comparing an acoustic three ring inlet and an...
The acoustic tests and data analysis for a 0.508-scale fan vehicle of a 111,300 newton (25,000 pound...
An analysis procedure was developed for design of acoustically treated nacelles for high bypass turb...
Acoustic and aerodynamic performance of six foot diameter fan for turbofan engines with noise suppre...
A set of long-chord stator vanes was designed to replace the vanes in an existing fan stage. The lon...
A set of acoustically-treated long-chord vanes was designed to replace the vanes in an existing fan ...
The effect of length of acoustic treatment was studied on a full scale fan using two different inlet...
Two inlet noise suppressors containing wall treatment plus three treated rings were tested on a fan ...
An advanced high bypass ratio fan model was tested in the NASA Lewis Research Center 9 x 15-Foot Low...
An existing fan stage was redesigned to reduce stator lift fluctuations and was acoustically tested ...
Concepts selected to reduce fan generated noise in a turbofan are presented. Near-sonic flow at the ...
Sound data which were obtained during tests of a 50.8 cm diameter, subsonic tip speed, low pressure ...
Tests of a 20 inch diameter, low tip speed, low pressure ratio fan which investigated aft fan noise ...
A study was made of the effect of increasing the fan rotor-to-stator spacing on the noise level of a...
Results of recent NASA research to reduce aircraft turbofan noise are described. As the bypass ratio...
The potential of two alternative approaches for reducing fan ton noise was investigated in this stud...
The acoustic tests and data analysis for a 0.508-scale fan vehicle of a 111,300 newton (25,000 pound...
An analysis procedure was developed for design of acoustically treated nacelles for high bypass turb...
Acoustic and aerodynamic performance of six foot diameter fan for turbofan engines with noise suppre...
A set of long-chord stator vanes was designed to replace the vanes in an existing fan stage. The lon...
A set of acoustically-treated long-chord vanes was designed to replace the vanes in an existing fan ...
The effect of length of acoustic treatment was studied on a full scale fan using two different inlet...
Two inlet noise suppressors containing wall treatment plus three treated rings were tested on a fan ...
An advanced high bypass ratio fan model was tested in the NASA Lewis Research Center 9 x 15-Foot Low...
An existing fan stage was redesigned to reduce stator lift fluctuations and was acoustically tested ...
Concepts selected to reduce fan generated noise in a turbofan are presented. Near-sonic flow at the ...
Sound data which were obtained during tests of a 50.8 cm diameter, subsonic tip speed, low pressure ...
Tests of a 20 inch diameter, low tip speed, low pressure ratio fan which investigated aft fan noise ...
A study was made of the effect of increasing the fan rotor-to-stator spacing on the noise level of a...
Results of recent NASA research to reduce aircraft turbofan noise are described. As the bypass ratio...
The potential of two alternative approaches for reducing fan ton noise was investigated in this stud...
The acoustic tests and data analysis for a 0.508-scale fan vehicle of a 111,300 newton (25,000 pound...
An analysis procedure was developed for design of acoustically treated nacelles for high bypass turb...
Acoustic and aerodynamic performance of six foot diameter fan for turbofan engines with noise suppre...