Abstract
The two-microphone method is investigated for the objective of in situ measuring the impedance of an acoustic liner In a duct. In order to avoid the influence caused by directly inserting the comparatively large microphones into a practical acoustic liner typically consisted of small honeycomb cells, the probe tubes as small as 1. 5 mm in diameter are used to conduct the sound pressure at the liner surface and that at the back plate to the microphones. A calibration method is designed to ensure high measurement accuracy of the thus-formed probe microphones. By the use of the two-microphone method, the acoustic impedance of a honeycomb-structure acoustic liner is measured when exposed to the sound waves at oblique incidences inside a duct. The measurement result is compared with the data obtained on a standard impedance tube and the prediction of an existing impedance model. The reliability of the present two-microphone method is validated by the good agreement between the different results.
| Original language | English |
|---|---|
| Pages (from-to) | 70-74 |
| Number of pages | 5 |
| Journal | Hangkong Dongli Xuebao/Journal of Aerospace Power |
| Volume | 23 |
| Issue number | 1 |
| State | Published - Jan 2008 |
Keywords
- Acoustic impedance measurement
- Acoustic liner
- Aerospace propulsion system
- Probe microphone
- Two-microphone method
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