Acoustic Performance of Drive Rig Mufflers for Model Scale Engine Testing
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Aircraft engine component testing at the NASA Glenn Research Center (GRC) includes acoustic testing of scale model fans and propellers in the 9- by15-Foot Low Speed Wind Tunnel (LSWT). This testing utilizes air driven turbines to deliver power to the article being studied. These air turbines exhaust directly downstream of the model in the wind tunnel test section and have been found to produce significant unwanted noise that reduces the quality of the acoustic measurements of the engine model being tested. This report describes an acoustic test of a muffler designed to mitigate the extraneous turbine noise. The muffler was found to provide acoustic attenuation of at least 8 dB between 700 Hz and 20 kHz which significantly improves the quality of acoustic measurements in the facility. Stephens, David, B. Glenn Research Center NASA/TM-2013-217885, E-18696
| Publisher Name | Independently Published |
|---|---|
| Author Name | Hagendorf, Col |
| Format | Audio |
| Bisac Subject Major | SCI |
| Language | NG |
| Isbn 10 | 179439740X |
| Isbn 13 | 9781794397408 |
| Target Age Group | min:NA, max:NA |
| Dimensions | 01.10" H x 00.08" L x 50.00" W |
| Page Count | 24 |
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