SpectraSim Documentation
Parameter · 05 Boundary Conditions

Grazing factor of a slit micro-perforate

perforate.grazing_factor Step 05 · Boundary Conditions

The factor of the grazing-flow resistance of a slit micro-perforated plate: grazing flow over the slits adds βM/σ\beta M/\sigma to the normalised resistance and leaves the reactance unchanged.

Last updated

Theory

A mean flow along the plate disturbs the oscillating flow in the slits and raises their acoustic resistance roughly in proportion to the grazing Mach number Kabral et al. (2014). The slit model of Guo et al. (2008), as given by Kabral et al. (2014) and Kabral (2015), adds the term βM/σ\beta M/\sigma to the resistance; the papers state that the reactance does not change with the flow.

The papers do not print a value of β\beta. The default 0.08 is derived from the authors' own model resistance at M=0.05M = 0.05 in Fig. 6 of Kabral et al. (2014) for both panels of their Table 2: the difference between that curve and the no-flow resistance of the same equations, times σ/M\sigma/M, gives 0.080 to 0.084 over the whole frequency range for both panels. The reading uncertainty of the figure is about ±0.01\pm 0.01. The same implementation reproduces the authors' reactance curves (their Fig. 7) to within the reading uncertainty.

Equations

rs=Re⁡{iωtσc[1−tanh⁡(ksi)ksi]−1}+4Rsσρc+β Mσr_s = \operatorname{Re}\left\{ \frac{i\omega t}{\sigma c}\left[1 - \frac{\tanh(k_s\sqrt{i})}{k_s\sqrt{i}}\right]^{-1} \right\} + \frac{4 R_s}{\sigma \rho c} + \beta\,\frac{M}{\sigma}
(1)
wheremeaningunit
rsr_sNormalised resistance of the slit plate-
ω\omegaAngular frequencyrad/s
ttPlate thicknessm
σ\sigmaOpen-area ratio-
ccSpeed of soundm/s
ksk_sShear wave number of the slit, bω/(4ν)b\sqrt{\omega/(4\nu)}-
RsR_sSurface resistance, 122ρωη\tfrac{1}{2}\sqrt{2\rho\omega\eta}Pa s/m
β\betaGrazing factor-
MMGrazing-flow Mach number-

Default and rule

Default
0.08 (derived from Kabral et al. 2014 Fig. 6, not printed in the paper)
Rule

0.08.

Source

Derived from the model curves of Kabral et al. (2014), Fig. 6, as described above; the equation is that of Kabral et al. (2014) (eqs. 2-5), from Guo et al. (2008).

Valid range 0 - 1; 0.08 +/- 0.01

Uncertainty

The default has a reading uncertainty of about ±0.01 from the figure.

Not printed

Where the panel maker or a measurement gives β, enter that value.

References 3

  1. Guo, Y., Allam, S. and Abom, M. (2008). Micro-perforated plates for vehicle applications. Proceedings of Inter-Noise 2008, 773-791. Web page
  2. 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
  3. Kabral, R. (2015). Aero-acoustic studies and innovative noise control with application to modern automotive gas exchange system. PhD thesis, Tallinn University of Technology, Theses on Mechanical Engineering E91, TUT Press. Web page