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Hydraulics, open channels and fluid power

Gravity-driven laminar film discharge per unit width

Discharge per unit width of a uniform laminar liquid film of thickness δ running down a plane inclined at θ above horizontal.

Ref
HYD-10
Rev
v1
Field
Hydraulics, open channels and fluid power
Result
q [m²/s]

A uniform liquid film running down a plane inclined at θ balances gravity along the plane against viscous shear, giving a parabolic velocity profile. The discharge per unit width is q = ρ g sinθ δ³/(3μ). It rises with the cube of the film thickness δ, so a slightly thicker film carries much more liquid. This assumes laminar flow and no shear at the free surface.

Discharge per unit width of a uniform laminar liquid film of thickness δ running down a plane inclined at θ above horizontal. The wall has no slip, and the free surface has no shear.

Calculator

Solve for
m²/s
kg/m³
5002,000
m/s²
130
°
0.590
m
1e-50.02
Pa·s
5e-410
  • Mean film velocity, q/δ0.1635 m/s
  • Free-surface velocity, ρ g sinθ δ²/(2μ)0.2452 m/s
  • Film Reynolds number, 4ρq/μ65.4

What drives the result

Each variable is moved across its typical range while the others stay at the values above. The longest bar is the key driver.

Discharge per unit width (m²/s) current value 1.635e-4 m²/s
δFilm thicknessKey driver
1.64e-101.31
μDynamic viscosity
1.63e-70.00327
gGravitational acceleration
1.67e-55e-4
θPlane angle above horizontal
2.85e-63.27e-4
ρLiquid density
8.17e-53.27e-4
  • The 1 mm film flows at a mean 0.1635 m/s, carrying 1.635×10−4 m²/s, or 0.1635 litres per second per metre of width.
  • The film Reynolds number is 65.4; the laminar formula holds only while it is low (roughly below 20 before waves develop).
Chart data as tables

Ranked variables

VariableTypical rangeLowest resultHighest resultSwing (m²/s)Local stepChange in result
δ Film thickness1e-5 to 0.02 m1.635e-101.3081.308+10%+33.1 %
μ Dynamic viscosity5e-4 to 10 Pa·s1.635e-70.003270.00327+10%−9.09 %
g Gravitational acceleration1 to 30 m/s²1.667e-55e-44.833e-4+10%+10 %
θ Plane angle above horizontal0.5 to 90 °2.854e-63.27e-43.241e-4+10%+8.93 %
ρ Liquid density500 to 2,000 kg/m³8.175e-53.27e-42.452e-4+10%+10 %

Sweep of Film thickness

Film thickness (m)Discharge per unit width (m²/s)
1e-51.635e-10
2.586e-52.828e-9
6.687e-54.89e-8
1.729e-48.456e-7
4.472e-41.462e-5
0.0011562.529e-4
0.0029910.004374
0.0077340.07563
0.021.308

Sweep one variable

Discharge per unit width (m²/s)Hover, touch, or use the arrow keys on the chart
00.51 1e−51e−40.0010.01 Film thickness (m), log scale now 1.635e-4

Variables and how each one contributes

q

Discharge per unit width

Result · m²/s

What the equation gives you. Everything else feeds it.

ρ

Liquid density

kg/m³ · typical 500 to 2,000

The liquid density, in kg/m³. Raises the discharge in direct proportion. Raising it by 10 % (to 1,100) moves the result by +10 %, from 1.635×10−4 to 1.798×10−4 m²/s.

g

Gravitational acceleration

m/s² · typical 1 to 30

The gravitational acceleration, in m/s². Raises the discharge in direct proportion. Raising it by 10 % (to 10.79) moves the result by +10 %, from 1.635×10−4 to 1.799×10−4 m²/s.

θ

Plane angle above horizontal

° · typical 0.5 to 90

The plane’s angle above horizontal, in degrees. A steeper plane raises the discharge in proportion to sin θ. Raising it by 10 % (to 33) moves the result by +8.93 %, from 1.635×10−4 to 1.781×10−4 m²/s.

δ

Film thickness

m · typical 1e-5 to 0.02

The film thickness, in m. Raises the discharge with the cube of the thickness. Raising it by 10 % (to 0.0011) moves the result by +33.1 %, from 1.635×10−4 to 2.176×10−4 m²/s.

μ

Dynamic viscosity

Pa·s · typical 5e-4 to 10

The dynamic viscosity, in Pa·s. A thicker liquid reduces the discharge in inverse proportion. Raising it by 10 % (to 0.011) moves the result by −9.09 %, from 1.635×10−4 to 1.486×10−4 m²/s.

Worked example with the values above

  1. Driving term: ρ g sinθ = 1,000 × 9.81 × 0.5 = 4,905 N/m³.
  2. Thickness term: δ³/(3μ) = 1×10−9 / (3 × 0.01) = 3.3333×10−8.
  3. q = 1.635×10−4 m²/s.

Assumptions and limits

  • Steady, fully developed laminar flow of a Newtonian liquid with no slip at the walls.
  • Smooth, straight geometry, and no body force other than gravity where stated.

Common mistakes

  • Using these results for turbulent flow, which has a flatter profile.
  • Entering the diameter where the radius is needed, which changes the answer by a factor of two or four.
  • Mixing the sign of the pressure gradient: it is −dp/dx, positive when pressure falls along the flow.

Statistics and uncertainty

These laminar formulas are exact for their model, so the uncertainty comes from the inputs. Gap and film thickness enter with the third power, so a 1 % error in thickness gives about a 3 % error in flow.

Where it is used

  • Lubrication films, coating, sealing gaps and thin-film runoff.
  • Checking viscous pipe flow and wall shear from measured pressure drops.

Maths you need

  • Viscosity: μ, the shear stress per unit velocity gradient
  • No-slip condition: the liquid moves with the wall at the wall
  • Reynolds number: the ratio of inertial to viscous forces

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