X-junction (P)#
Block appearance in REPEAT VISION#
The X-junction (P) block models the intersection of four branches of a pneumatic network at an angle of 90\(^o\).
Fig. 1 Flow converging to vertex C#
Fig. 2 Flow diverging from vertex C#
Hint
The AC branch is the main one, the BD branch is the side one.
1. Calculation of loss coefficients#
With this setting, the user directly sets dimensionless loss coefficients for converging and diverging, perpendicular and counter flows:
divLossCoef– when three flows making part of an assembly merge into one common flow in the direction of the fourth vertex of the junction:
Fig. 3 Three flows making part of an assembly merge into one common flow in the direction of the fourth junction vertex#
convLossCoef– when an incoming flow on one of the vertices diverges into three flows towards the other three vertices:
Fig. 4 The incoming flow on one of the vertices diverges into three flows towards the other three vertices#
perpLossCoef- when the two flows entering the assembly are perpendicular and the two outgoing flows are perpendicular to the incoming ones and each other:
Fig. 5 The two flows entering the assembly are perpendicular and the two outgoing flows are perpendicular to the incoming ones and each other#
collLossCoef- for the case when two flows entering the assembly are opposite, and two outgoing flows form an angle of 90\(^о\):
Fig. 6 The two flows entering the assembly are opposite, and the two outgoing flows form an angle of 90° with the incoming flow#
Mass conservation equation(1) :
Pressure drop calculation (2) :
where:
\(I=A, B, C, D\);
\(A_i\) – cross-sectional area of branch I, [m\(^2\)];
\(K_i\) – dimensionless loss factors on branch I;
\(I_i\) – gas inertia on branch I;
\(m_i\) – mass flow rate of gas through port I, [kg/s].
\(m_{thresh}\) – threshold flow rate, below which the flow is considered stagnant and cannot be defined as converging or diverging. Calculated using the following formula (3) :
where:
\(A_{min}\) – minimum area of the side and main branches, m\(^2\);
\( ho\) – gas density, [kg/m\(^3\)];
\( u\) – kinematic viscosity of gas, [mm\(^2\)/s].
Calculation of inertia (4), (5), (6), (7) :
2. Properties#
Property |
Default Value |
Description |
Units of measurement |
|---|---|---|---|
Main branch AC area |
0.01 |
- |
m\(^2\) |
Side branch BD area |
0.01 |
- |
m\(^2\) |
Critical Reynolds number |
150.0 |
- |
- |
Loss coefficient for divergence flows (from 1 to 3) |
1.12 |
- |
- |
Loss coefficient for convergence flows (from 3 to 1) |
1.12 |
- |
- |
Loss coefficient for perpendicular flows (from 2 to 2) |
1.12 |
- |
- |
Loss coefficient for colliding flows (from 2 to 2) |
1.12 |
- |
- |
3. Inputs and outputs#
Parameters |
Input/Output |
Description |
Units of measurement |
Port type |
|---|---|---|---|---|
Port A |
Input |
- |
- |
Pneumatics |
Port B |
Input |
- |
- |
Pneumatics |
Port С |
Input |
- |
- |
Pneumatics |
Port D |
Input |
- |
- |
Pneumatics |
In order to see the connection capabilities of the block, you need to go to page Description of block ports