Theory
The aperture enters the linear flow term as (or ), so a small change of it changes the pressure drop much: 10 % smaller holes give 23 % more viscous loss Maa (1998) Kabral et al. (2014).
Equations
(1)
| where | meaning | unit |
|---|---|---|
| Pressure jump across the wall | Pa | |
| Velocity through the wall face | m/s | |
| Wall thickness | m | |
| Inertial coefficient | 1/m |
Default and rule
- Default
- 0.2 mm
- Rule
0.2 mm.
- Source
Maa (1998) eq. 3a; Kabral et al. (2014) eq. 2; Allam and Abom (2011) eq. 23 (inertial term).
Valid range 0.05 - 1 mm (the micro-perforate models' range)
Sub-millimetre
Above about 1 mm the holes are no longer micro-perforations: use the perforated-tube or plate type.
Related 5
References 3
- Allam, S. and Abom, M. (2011). A new type of muffler based on microperforated tubes. Journal of Vibration and Acoustics, 133(3), 031005. DOI 10.1115/1.4002956
- Kabral, R., Du, L., Abom, M. and Knutsson, M. (2014). A compact silencer for the control of compressor noise. SAE International Journal of Engines, 7(3), 1572-1578. DOI 10.4271/2014-01-2060
- Maa, D.-Y. (1998). Potential of microperforated panel absorber. Journal of the Acoustical Society of America, 104(5), 2861-2866. DOI 10.1121/1.423870