The Structural Acoustics Loads and Transmission (SALT) facility at the NASA Langley Research Center is comprised of an anechoic room and a reverberant room, and may act as a transmission loss suite when test articles are mounted in a window connecting the two rooms. In the latter configuration, the reverberant room acts as the noise source side and the anechoic room as the receiver side. The noise generation system used for qualification testing in the reverberant room was previously shown to achieve a maximum overall sound pressure level of 141 dB. This is considered to be marginally adequate for generating sound pressure levels typically required for launch vehicle payload qualification testing. Recent enhancements to the noise generation...
The design, construction, and costs of a test facility for determining the sound transmission loss c...
Design, construction, and performance of manned space center acoustic laboratory for ground tests of...
Measurements were made in the no. 1 7'x10' wind tunnel at NASA Ames Research Center, with the object...
It is important to realize that some test-articles may have significant sound absorption that may ch...
The exposure of a customer's aerospace test-article to a simulated acoustic launch environment is ty...
The Acoustical Testing Laboratory (ATL) consists of a 27 by 23 by 20 ft (height) convertible hemi/an...
A description of the Transmission Loss Apparatus at NASA Langley Research Center, which is specifica...
An initial acoustic calibration was performed for the NASA Langley Research Center reverberation cha...
The exposure of a customers aerospace test-article to a simulated acoustic launch environment is typ...
A recent operational need for the development of a large (101,000 ft 3) reverberant acoustic chamber...
The NASA John H. Glenn Research Center at Lewis Field has designed and constructed an Acoustical Tes...
A facility has been constructed at NASA Langley Research Center to simulate the soundscape inside re...
NASA Lewis Research Center recently led a multi-organizational acoustic test program. This testing c...
The full-scale wind tunnel at NASA-Langley Research Center was designed for low-speed aerodynamic te...
A technique to measure the radiated acoustic intensity and transmission loss of panels is documented...
The design, construction, and costs of a test facility for determining the sound transmission loss c...
Design, construction, and performance of manned space center acoustic laboratory for ground tests of...
Measurements were made in the no. 1 7'x10' wind tunnel at NASA Ames Research Center, with the object...
It is important to realize that some test-articles may have significant sound absorption that may ch...
The exposure of a customer's aerospace test-article to a simulated acoustic launch environment is ty...
The Acoustical Testing Laboratory (ATL) consists of a 27 by 23 by 20 ft (height) convertible hemi/an...
A description of the Transmission Loss Apparatus at NASA Langley Research Center, which is specifica...
An initial acoustic calibration was performed for the NASA Langley Research Center reverberation cha...
The exposure of a customers aerospace test-article to a simulated acoustic launch environment is typ...
A recent operational need for the development of a large (101,000 ft 3) reverberant acoustic chamber...
The NASA John H. Glenn Research Center at Lewis Field has designed and constructed an Acoustical Tes...
A facility has been constructed at NASA Langley Research Center to simulate the soundscape inside re...
NASA Lewis Research Center recently led a multi-organizational acoustic test program. This testing c...
The full-scale wind tunnel at NASA-Langley Research Center was designed for low-speed aerodynamic te...
A technique to measure the radiated acoustic intensity and transmission loss of panels is documented...
The design, construction, and costs of a test facility for determining the sound transmission loss c...
Design, construction, and performance of manned space center acoustic laboratory for ground tests of...
Measurements were made in the no. 1 7'x10' wind tunnel at NASA Ames Research Center, with the object...