Plane Couette and Poiseuille flow interact by superposition: surface motion produces a linear Couette velocity profile, while the pressure gradient adds a parabolic Poiseuille contribution. In a converging thin-film rig with equal ambient pressure at the inlet and outlet, the moving wall carries fluid into the narrowing gap, creating a pressure rise; the maximum pressure occurs in the downstream half, where the pressure gradient changes sign.
In a converging slider film, Couette drag supplies the fluid transport and the resulting pressure-driven Poiseuille component adjusts the flow rate and velocity profile. For a monotonic linear gap with equal inlet and outlet pressures, the pressure peak lies at (x/L > 0.5), although its exact location depends on the gap ratio.
How the Two Flow Components Combine
Plane Couette Flow Comes From Wall Motion
Plane Couette flow is generated when one surface moves relative to the other. If the moving surface has speed (U), the shear-driven velocity component varies approximately linearly across the film thickness.
For a stationary lower wall and a moving upper wall, the ideal Couette contribution is
[ u_C(y)=U\frac{y}{h}, ]
where (h) is the local gap height and (y) measures distance across the gap.
Plane Poiseuille Flow Comes From Pressure Gradient
A pressure gradient adds a pressure-driven component with a parabolic profile:
[ u_P(y)=-\frac{1}{2\mu}\frac{dP}{dx}y(h-y), ]
where (\mu) is the dynamic viscosity.
The sign of (dP/dx) determines whether this component assists or opposes the wall-driven transport. A positive downstream pressure rise generally creates a pressure-driven component opposing the net Couette flow.
The Actual Profile Is Their Sum
Under the usual thin-film assumptions, the local velocity is the superposition
[ u(y)=U\frac{y}{h} -\frac{1}{2\mu}\frac{dP}{dx}y(h-y). ]
The resulting profile is therefore neither purely linear nor purely parabolic. The pressure gradient bends the Couette profile, altering both the velocity distribution and the volumetric flow rate.
Why a Converging Gap Builds Pressure
Wall Motion Carries Fluid Into the Wedge
In a converging slider gap, the wall drags fluid downstream while the available cross-sectional area decreases. If the pressure remained uniform, the downstream flow would not generally satisfy continuity.
The fluid must adjust its velocity and pressure so that the same steady mass flow passes through every cross-section.
The Pressure Gradient Opposes Excess Transport
The developing pressure gradient produces a Poiseuille component that counteracts the amount of fluid that Couette motion would otherwise push into the narrowing region.
This is the central interaction in a demonstration rig: Couette flow provides the pumping action, while Poiseuille flow provides the pressure-driven correction required by continuity.
Pressure Rises and Then Falls
With equal ambient pressures imposed at the inlet and outlet, pressure cannot rise indefinitely. It increases through the upstream portion of the wedge, reaches a maximum, and then decreases toward the outlet pressure.
At the pressure maximum,
[ \frac{dP}{dx}=0. ]
The local velocity profile is then purely Couette-shaped at that exact cross-section, although the flow elsewhere contains both components.
Where Maximum Pressure Occurs
The Peak Is Downstream of the Midpoint
For a linearly converging gap whose larger opening is at (x=0) and smaller opening at (x=L), the pressure maximum occurs in the downstream half:
[ \frac{x_{\text{max}}}{L}>0.5. ]
The exact position is controlled by the ratio of the inlet and outlet gaps, not simply by the geometric midpoint.
Location for a Linear Wedge
Let the inlet and outlet gaps be (h_i) and (h_o), respectively, with (h_i>h_o). For the standard idealized case of equal inlet and outlet pressures, the pressure maximum occurs where the local gap is approximately
[ h_{\text{max}}=\frac{2h_i h_o}{h_i+h_o}. ]
For a linear gap variation, this corresponds to
[ \frac{x_{\text{max}}}{L}=\frac{h_i}{h_i+h_o}. ]
Because (h_i>h_o), this ratio is greater than one-half. A stronger convergence ratio generally shifts the pressure peak farther downstream.
What Happens at the Peak
At the peak, the pressure gradient is zero, so the pressure-driven Poiseuille contribution vanishes locally. Upstream of the peak, the pressure rises in the direction of motion; downstream, it falls toward the outlet pressure.
The pressure itself remains substantial at the peak even though its local gradient is zero. A zero gradient means the pressure is stationary with respect to position, not that the pressure is zero.
What a Demonstration Rig Shows
Velocity Profiles Change Across the Film
Near the inlet, the flow is strongly influenced by wall drag and the developing pressure field. As pressure builds, the parabolic Poiseuille component increasingly modifies the linear Couette profile.
In the region where the pressure-driven component opposes the wall motion, the profile may become less uniformly downstream-directed and can develop a locally reduced or even reversed velocity near one wall, depending on the operating conditions.
Pressure Taps Reveal the Wedge Effect
Pressure taps along the converging plate should show a pressure rise followed by a fall when inlet and outlet pressures are equal. The highest tap reading should therefore occur after the geometric midpoint under the stated assumptions.
The measured location may differ from the ideal prediction because of inlet development, leakage, surface alignment errors, finite-width effects, cavitation, or nonuniform gap spacing.
Viscosity and Speed Affect Pressure Magnitude
The pressure buildup increases with fluid viscosity and relative surface speed, and it is highly sensitive to the gap geometry. Small changes in the minimum gap can produce large changes in the predicted pressure because thin-film pressure generation depends strongly on powers of the local film thickness.
The pressure distribution is therefore a useful demonstration of how mechanical motion can generate a pressure field without an externally imposed pump pressure gradient.
Understanding the Trade-offs
The Downstream-Half Rule Has Conditions
The statement that the pressure peak is always downstream of the midpoint applies to the ideal converging planar slider with a monotonic linear gap, steady motion, equal ambient endpoint pressures, and the standard thin-film assumptions.
It should not be applied automatically to stepped, curved, nonmonotonic, porous, heavily leaking, or cavitating films. Different boundary pressures can also move the maximum or eliminate an interior maximum.
Pressure Magnitude Is Not Determined by Speed Alone
Higher surface velocity does not specify a unique pressure rise. The result also depends on viscosity, inlet and outlet gaps, wedge length, and the exact boundary conditions.
Comparing rigs solely by wall speed can therefore be misleading if their gap ratios or fluids differ.
Ideal Superposition Has Limits
Couette-Poiseuille superposition describes the local laminar velocity field when inertia is small and the fluid behaves approximately as a Newtonian liquid. Turbulence, non-Newtonian rheology, thermal effects, three-dimensional side leakage, and surface roughness require additional modeling.
The ideal result remains valuable because it isolates the mechanism, but the apparatus may display deviations from the one-dimensional prediction.
How to Apply This to Your Project
Use the following checks when interpreting a thin-film demonstration rig:
- If your primary focus is velocity profiles: Treat the measured flow as a linear Couette contribution plus a parabolic Poiseuille contribution controlled by (dP/dx).
- If your primary focus is pressure location: For a monotonic linear converging gap with equal endpoint pressures, look for the maximum in the downstream half, at (x/L>0.5).
- If your primary focus is pressure magnitude: Compare viscosity, surface speed, film length, and inlet-to-outlet gap ratio together rather than considering any one variable in isolation.
- If your primary focus is experimental accuracy: Check alignment, leakage, cavitation, endpoint pressures, and whether the gap is genuinely linear before comparing measurements with the ideal model.
The essential principle is that wall motion drives Couette transport, pressure gradients create the Poiseuille correction, and a converging gap converts their interaction into a downstream pressure maximum.
Summary Table:
| Key aspect | Main insight |
|---|---|
| Couette flow | Wall motion creates a linear velocity profile and transports fluid downstream. |
| Poiseuille flow | Pressure gradients add a parabolic flow component that adjusts transport. |
| Pressure peak | At the maximum, dP/dx = 0 and the local profile is purely Couette-shaped. |
| Peak location | For a linear converging gap with equal endpoint pressures, x/L > 0.5. |
| Peak-gap relation | h_max = 2h_i h_o / (h_i + h_o); x_max/L = h_i / (h_i + h_o). |
| Pressure magnitude | Depends on viscosity, surface speed, wedge length, gap ratio, and boundary conditions. |
| Experimental effects | Leakage, cavitation, misalignment, side effects, and nonuniform gaps can shift results. |
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