Orifice Plate: Single and Multi-Stage Pressure Drop
The orifice plate is a canonical internal flow benchmark for pressure drop across a constriction. This case sweeps four configurations of increasing complexity: a single plate with one centered opening, a single plate with three evenly spaced openings, and two- and three-plate staggered arrangements where the openings alternate between the upper and lower channel to force a serpentine flow path.
These configurations have direct industrial applications in flow metering (ISO 5167 orifice plates), labyrinth seals in turbomachinery, baffled heat exchangers, and muffler/silencer systems. The multi-stage cases provide a clear validation target: the total loss coefficient should scale approximately as N times the single-plate loss, with additional turning losses from the serpentine path.
Setup
| Parameter | Value |
|---|---|
| Grid | 1600 × 1000 |
| Configurations | 1p1h, 1p3h, 2p, 3p |
| Plate thickness | 8 cells (max(4, NX/100)) |
| Hole width | 125 cells (NY/8) |
| Reynolds number | 100 |
| Inlet velocity | uinflow = 0.025 lu/ts |
| Tau (relaxation parameter) | 1.25 |
| Number of steps | 30,000 |
| Reference length | H = NY = 1000 cells (channel height) |
| Collision | MRT (d'Humieres 2002) |
| Boundary condition | Zou-He inlet, convective outlet, bounce-back plates |
| Lattice spacing / time step | Δx = 1, Δt = 1 |
Flow Field
Use the tabs below to select a parameter variant. Top left: steady-state velocity contour with streamlines. Top right: flow evolution from rest to steady state. Bottom: pressure and vorticity fields at steady state.
Velocity (Contour | Streamlines)
Drag the handle to wipe between the velocity-magnitude contour and the streamline plot.
Flow Evolution
Pressure Coefficient Cp
Pressure Coefficient Cp
Vorticity
Vorticity
Validation
| Config | Re | Computed Fx | Loss Coeff K | Regime |
|---|---|---|---|---|
| 1 plate, 1 hole | 100 | 13.1 | 139 | Classic single orifice |
| 1 plate, 3 holes | 100 | 0.97 | 10.4 | Perforated baffle (lowest loss) |
| 2 plates | 100 | 30.4 | 324 | Single serpentine turn |
| 3 plates | 100 | 54.0 | 575 | Double serpentine turn (highest loss) |
Discussion
The staggered orifice plate configuration exercises the solver's ability to handle multiple internal solid boundaries with confined flow passages. Unlike external aerodynamics cases where the flow can freely divert around obstacles, the serpentine path forces the fluid through narrow gaps at alternating elevations. This creates a complex flow pattern with:
- Sudden contraction/expansion at each plate entrance/exit
- 180-degree turning flow between stages
- Confined jet impingement on the channel walls
- Recirculation zones in the blind corners behind each plate
The pressure drop across each stage depends on the contraction ratio (hole area / channel area), the Reynolds number, and the inter-stage spacing. For design purposes, the total loss is approximated as:
where K_orifice is the single-orifice loss coefficient and K_turn accounts for the 180-degree turning loss between stages. At high Re, K_turn dominates due to momentum-driven separation; at low Re (laminar), viscous friction in the inter-stage passages adds significant losses. This case serves as a validation bridge between simple orifice metering (ISO 5167) and complex labyrinth seal flows in turbomachinery.