Modelica.Fluid.Dissipation.Utilities.SharedDocumentation.PressureLoss.Orifice Modelica.Fluid.Dissipation.Utilities.SharedDocumentation.PressureLoss.Orifice

Extends from Modelica.Icons.Information (Icon for general information packages).

Package Content

Name Description
Modelica.Fluid.Dissipation.Utilities.SharedDocumentation.PressureLoss.Orifice.dp_suddenChange dp_suddenChange  
Modelica.Fluid.Dissipation.Utilities.SharedDocumentation.PressureLoss.Orifice.dp_thickEdgedOverall dp_thickEdgedOverall  

Modelica.Fluid.Dissipation.Utilities.SharedDocumentation.PressureLoss.Orifice.dp_suddenChange Modelica.Fluid.Dissipation.Utilities.SharedDocumentation.PressureLoss.Orifice.dp_suddenChange

Restriction

This function shall be used within the restricted limits according to the referenced literature.

Geometry

pic_suddenChangeSection

Calculation

The local pressure loss dp is generally determined by:

    dp = 0.5 * zeta_LOC * rho * |v_1|*v_1

with

rho as density of fluid [kg/m3],
v_1 as average flow velocity in small cross sectional area [m/s].
zeta_LOC as local resistance coefficient [-],

The local resistance coefficient zeta_LOC of a sudden expansion can be calculated for different ratios of cross sectional areas by:

    zeta_LOC = (1 - A_1/A_2)^2  [Idelchik 2006, p. 208, diag. 4-1] 

and for sudden contraction:

    zeta_LOC = 0.5*(1 - A_1/A_2)^0.75  [Idelchik 2006, p. 216-217, diag. 4-9] 

with

A_1 small cross sectional area [m^2],
A_2 large cross sectional area [m^2].

Verification

The local resistance coefficient zeta_LOC of a sudden expansion in dependence of the cross sectional area ratio A_1/A_2 is shown in the figure below.

fig_orifice_suddenChangeExpansion

The local resistance coefficient zeta_LOC of a sudden contraction in dependence of the cross sectional area ratio A_1/A_2 is shown in the figure below.

fig_orifice_suddenChangeContraction

References

Elmqvist, H., M.Otter and S.E. Cellier:
Inline integration: A new mixed symbolic / numeric approach for solving differential-algebraic equation systems.. In Proceedings of European Simulation MultiConference, Praque, 1995.
Idelchik,I.E.:
Handbook of hydraulic resistance. Jaico Publishing House, Mumbai, 3rd edition, 2006.

Extends from Modelica.Icons.Information (Icon for general information packages).

Modelica.Fluid.Dissipation.Utilities.SharedDocumentation.PressureLoss.Orifice.dp_thickEdgedOverall Modelica.Fluid.Dissipation.Utilities.SharedDocumentation.PressureLoss.Orifice.dp_thickEdgedOverall

Restriction

This function shall be used within the restricted limits according to the referenced literature.

Geometry

pic_thickEdged

Calculation

The pressure loss dp for a thick edged orifice is determined by:

    dp = zeta_TOT * (rho/2) * (velocity_1)^2

with

rho as density of fluid [kg/m3],
velocity_1 as mean velocity in large cross sectional area [m/s],
zeta_TOT as pressure loss coefficient [-].

The pressure loss coefficient zeta_TOT of a thick edged orifice can be calculated for different cross sectional areas A_0 and relative length of orifice l_bar =L/d_hyd_0 by:

    zeta_TOT = (0.5*(1 - A_0/A_1)^0.75 + tau*(1 - A_0/A_1)^1.375 + (1 - A_0/A_1)^2 + lambda_FRI*l_bar)*(A_1/A_0)^2 [Idelchik 2006, p. 222, diag. 4-15] 

with

A_0 cross sectional area of vena contraction [m2],
A_1 large cross sectional area of orifice [m2],
d_hyd_0 hydraulic diameter of vena contraction [m],
lambda_FRI as constant Darcy friction factor [-],
l_bar relative length of orifice [-],
L length of vena contraction [m],
tau geometry parameter [-].

The geometry factor tau is determined by [Idelchik 2006, p. 219, diag. 4-12]:

    tau = (2.4 - l_bar)*10^(-phi)
    phi = 0.25 + 0.535*l_bar^8 / (0.05 + l_bar^8) .

Verification

The pressure loss coefficient zeta_TOT of a thick edged orifice in dependence of a relative length (l_bar = L /d_hyd) with different ratios of cross sectional areas A_0/A_1 is shown in the figure below.

fig_orifice_thickEdgedOverall_ZETAvsLENGTH

Incompressible case [Pressure loss = f(m_flow)]:

The pressure loss DP of an thick edged orifice in dependence of the mass flow rate m_flow of water for different ratios A_0/A_1 (where A_0 = 0.001 m^2) is shown in the figure below.

fig_orifice_thickEdgedOverall_DPvsMFLOW

And for the compressible case [Mass flow rate = f(dp)]:

fig_orifice_thickEdgedOverall_MFLOWvsDP

References

Elmqvist,H., M.Otter and S.E. Cellier:
Inline integration: A new mixed symbolic / numeric approach for solving differential-algebraic equation systems.. In Proceedings of European Simulation MultiConference, Praque, 1995.
Idelchik,I.E.:
Handbook of hydraulic resistance. Jaico Publishing House,Mumbai, 3rd edition, 2006.

Extends from Modelica.Icons.Information (Icon for general information packages).

Automatically generated Thu Dec 19 17:20:12 2019.