SpectraSim Documentation
Parameter · 05 Boundary Conditions

Discharge coefficient C_D0

perforate.tube_discharge_coefficient Step 05 · Boundary Conditions

The discharge coefficient of the holes of a perforated tube without grazing flow: the ratio of the actual flow rate through a hole to the ideal flow rate at the same pressure difference. It sets the initial loss coefficient K0=1/(σCD0)2K_0 = 1/(\sigma C_{D0})^2 and is the upper limit of the grazing-flow discharge coefficient.

Last updated

Theory

A jet leaving a sharp-edged hole contracts, so it carries less flow than the hole area multiplied by the ideal velocity; CDC_D quantifies this reduction. For a thin plate CDC_D is typically 0.6-0.7; in a thicker wall the jet partly reattaches inside the bore, which raises the coefficient.

On Auto, the program interpolates bilinearly, equation (1), in a table of measured steady-flow discharge coefficients:

  • rows of wall thickness tt = 0.5, 0.8, 1.0, 1.25, 1.5, 2.0 and 2.5 mm;
  • columns of hole diameter dd from 0.6 to 5 mm;
  • values between 0.72 and 0.91.

Outside the table the nearest edge value is used; the program never extrapolates beyond the table.

With the grazing correction enabled (Grazing correction), the coefficient applied on each face is min⁡(CDe,CD0)\min(C_{De}, C_{D0}): grazing flow lowers the coefficient, and as the grazing flow becomes small it returns to CD0C_{D0}. In a flow + acoustics run the same value is used as the acoustic model's CDC_D (Discharge coefficient C_D (acoustics)).

Equations

CD0=∑a,b∈{0,1}wa(t) wb(d) Ci+a, j+b,K0=1(σ CD0)2C_{D0} = \sum_{a,b \in \{0,1\}} w_a(t)\,w_b(d)\,C_{i+a,\,j+b}, \qquad K_0 = \frac{1}{(\sigma\,C_{D0})^2}
(1)
wheremeaningunit
Ci,jC_{i,j}Table value at thickness row ii and diameter column jj bracketing (t,d)(t, d)-
wa,wbw_a, w_bLinear interpolation weights in tt and dd (clamped to the table)-
σ\sigmaOpen-area ratio-
K0K_0Initial loss coefficient-

Default and rule

Default
Auto: interpolated in the hole-diameter × wall-thickness tableComputed by the program
Rule

Auto (table interpolation). A value between 0.05 and 1 entered by the user overrides the table.

Source

The table contains Elnady's measured DC-flow discharge coefficients as a function of hole diameter and wall thickness: Table 1 of Paper III (Elnady and Boden, 2004) of his doctoral thesis (Elnady, 2004); the related journal paper is (Elnady et al., 2010). The measured samples cover dd = 0.6-2.4 mm and tt = 0.8-2.4 mm; the remainder of the table is Elnady's extrapolation. The table values are not reproduced here; refer to the thesis.

Valid range 0.05 ≤ C_D0 ≤ 1

Values

0.05 to 1. A user value replaces the table for the CFD and, in a flow + acoustics run, for the acoustic model.

Extrapolated table cells

Outside dd = 0.6-2.4 mm or tt = 0.8-2.4 mm the table value is Elnady's extrapolation; the boundary-condition card indicates this.

References 3

  1. Elnady, T. (2004). Modelling and characterization of perforates in lined ducts and mufflers. Doctoral thesis, KTH Royal Institute of Technology, Stockholm (Paper III, Table 1). Web page
  2. Elnady, T., Åbom, M. and Allam, S. (2010). Modeling perforates in mufflers using two-ports. Journal of Vibration and Acoustics, 132(6), 061010. DOI 10.1115/1.4001510
  3. Elnady, T. and Boden, H. (2004). On the modelling of the acoustic impedance of perforates with flow. Paper III of T. Elnady, Modelling and characterization of perforates in lined ducts and mufflers, doctoral thesis, KTH Royal Institute of Technology, Stockholm. Web page