Add to ORKGThe 9- by 15-Foot Low Speed Wind Tunnel has been used for acoustic testing for more than 40 years. The facility is principally used for testing aircraft engine propulsion components, for both aerodynamic performance and acoustics. The present report discusses the instrumentation and procedures currently used for the acquisition of high-quality acoustic data from aircraft engine fan models
The 9- by 15-Foot Low Speed Wind Tunnel (9x15 LSWT) at NASA Glenn Research Center was built in 1969 ...
A wind tunnel experiment was conducted in the NASA Glenn Research Center anechoic 9- by 15-Foot Low-...
In an effort to identify test facilities that offer sonic boom measurement capabilities, an explorat...
The 9- by 15-Foot Low Speed Wind Tunnel is an acoustic testing facility with a long history of aircr...
A comprehensive aeroacoustic research program called the Source Diagnostic Test was recently conclud...
Methods are presented for making overall and directional acoustic measurements with forward velocity...
Prior to the NASA Glenn Research Center 9- by 15-Foot Low-Speed Wind Tunnel (9x15 LSWT) undergoing s...
The 9- by 15-Foot Low Speed Wind Tunnel (9x15 LSWT) at NASA Glenn Research Center was built in 1969 ...
The test section of the NASA Lewis 9- by 15-Foot Low Speed Wind Tunnel was acoustically treated to a...
A Williams International FJ44-3A 3000-lb thrust class turbofan engine was tested in the NASA Glenn R...
In February 2017, aerodynamic and acoustic testing was completed on a scale-model high bypass ratio ...
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 (9x15 LSWT) at NASA Glenn Research Center was built in 1969 ...
Far-field acoustic power level and performance analyses of open rotor model F31/A31 have been perfor...
The Acoustical Testing Laboratory (ATL) consists of a 27- by 23- by 20-ft (height) convertible hemi/...
The 9- by 15-Foot Low Speed Wind Tunnel (9x15 LSWT) at NASA Glenn Research Center was built in 1969 ...
A wind tunnel experiment was conducted in the NASA Glenn Research Center anechoic 9- by 15-Foot Low-...
In an effort to identify test facilities that offer sonic boom measurement capabilities, an explorat...
The 9- by 15-Foot Low Speed Wind Tunnel is an acoustic testing facility with a long history of aircr...
A comprehensive aeroacoustic research program called the Source Diagnostic Test was recently conclud...
Methods are presented for making overall and directional acoustic measurements with forward velocity...
Prior to the NASA Glenn Research Center 9- by 15-Foot Low-Speed Wind Tunnel (9x15 LSWT) undergoing s...
The 9- by 15-Foot Low Speed Wind Tunnel (9x15 LSWT) at NASA Glenn Research Center was built in 1969 ...
The test section of the NASA Lewis 9- by 15-Foot Low Speed Wind Tunnel was acoustically treated to a...
A Williams International FJ44-3A 3000-lb thrust class turbofan engine was tested in the NASA Glenn R...
In February 2017, aerodynamic and acoustic testing was completed on a scale-model high bypass ratio ...
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 (9x15 LSWT) at NASA Glenn Research Center was built in 1969 ...
Far-field acoustic power level and performance analyses of open rotor model F31/A31 have been perfor...
The Acoustical Testing Laboratory (ATL) consists of a 27- by 23- by 20-ft (height) convertible hemi/...
The 9- by 15-Foot Low Speed Wind Tunnel (9x15 LSWT) at NASA Glenn Research Center was built in 1969 ...
A wind tunnel experiment was conducted in the NASA Glenn Research Center anechoic 9- by 15-Foot Low-...
In an effort to identify test facilities that offer sonic boom measurement capabilities, an explorat...
