The Acoustical Testing Laboratory (ATL) consists of a 27 by 23 by 20 ft (height) convertible hemi/anechoic chamber and separate sound-attenuating test support enclosure. Absorptive fiberglass wedges in the test chamber provide an anechoic environment down to 100 Hz. A spring-isolated floor system affords vibration isolation above 3 Hz. These specifications, along with very low design background levels, enable the acquisition of accurate and repeatable acoustical measurements on test articles that produce very low sound pressures. Removable floor wedges allow the test chamber to operate in either a hemi-anechoic or anechoic configuration, depending on the size of the test article and the specific test being conducted. The test support enclos...
The exposure of a customer's aerospace test-article to a simulated acoustic launch environment is ty...
The acoustic capability of the NASA Lewis 9 by 15 Foot Low Speed Wind Tunnel has been significantly ...
An initial acoustic calibration was performed for the NASA Langley Research Center reverberation cha...
The Acoustical Testing Laboratory (ATL) consists of a 27- by 23- by 20-ft (height) convertible hemi/...
The NASA John H. Glenn Research Center at Lewis Field has designed and constructed an Acoustical Tes...
NASA Glenn Research Center's Acoustical Testing Laboratory (ATL) provides a comprehensive array of a...
A new acoustic arena has been qualified in the Aero-Acoustic Propulsion Laboratory (AAPL) at the NAS...
The 9- by 15-Foot Low Speed Wind Tunnel is an acoustic testing facility with a long history of aircr...
The Structural Acoustics Loads and Transmission (SALT) facility at the NASA Langley Research Center ...
The full-scale wind tunnel at NASA-Langley Research Center was designed for low-speed aerodynamic te...
NASA Lewis Research Center recently led a multi-organizational acoustic test program. This testing c...
It is important to realize that some test-articles may have significant sound absorption that may ch...
The NASA Flight Effects Program has a requirement to compare acoustic data obtained from flyover, st...
The exposure of a customers aerospace test-article to a simulated acoustic launch environment is typ...
The 9- by 15-Foot Low Speed Wind Tunnel (9x15 LSWT) at NASA Glenn Research Center was built in 1969 ...
The exposure of a customer's aerospace test-article to a simulated acoustic launch environment is ty...
The acoustic capability of the NASA Lewis 9 by 15 Foot Low Speed Wind Tunnel has been significantly ...
An initial acoustic calibration was performed for the NASA Langley Research Center reverberation cha...
The Acoustical Testing Laboratory (ATL) consists of a 27- by 23- by 20-ft (height) convertible hemi/...
The NASA John H. Glenn Research Center at Lewis Field has designed and constructed an Acoustical Tes...
NASA Glenn Research Center's Acoustical Testing Laboratory (ATL) provides a comprehensive array of a...
A new acoustic arena has been qualified in the Aero-Acoustic Propulsion Laboratory (AAPL) at the NAS...
The 9- by 15-Foot Low Speed Wind Tunnel is an acoustic testing facility with a long history of aircr...
The Structural Acoustics Loads and Transmission (SALT) facility at the NASA Langley Research Center ...
The full-scale wind tunnel at NASA-Langley Research Center was designed for low-speed aerodynamic te...
NASA Lewis Research Center recently led a multi-organizational acoustic test program. This testing c...
It is important to realize that some test-articles may have significant sound absorption that may ch...
The NASA Flight Effects Program has a requirement to compare acoustic data obtained from flyover, st...
The exposure of a customers aerospace test-article to a simulated acoustic launch environment is typ...
The 9- by 15-Foot Low Speed Wind Tunnel (9x15 LSWT) at NASA Glenn Research Center was built in 1969 ...
The exposure of a customer's aerospace test-article to a simulated acoustic launch environment is ty...
The acoustic capability of the NASA Lewis 9 by 15 Foot Low Speed Wind Tunnel has been significantly ...
An initial acoustic calibration was performed for the NASA Langley Research Center reverberation cha...