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Hydraulics, open channels and fluid power

Diameter of a falling free liquid jet

Diameter of a vertical circular jet after it has fallen a distance H from a section of diameter d₁ and speed U₁, from continuity and Bernoulli at atmospheric pressure, with no drag, break-up or surface tension.

Ref
HYD-35
Rev
v1
Field
Hydraulics, open channels and fluid power
Result
d2 [m]

A liquid jet falling vertically speeds up, and continuity makes it narrow. Bernoulli at atmospheric pressure gives the speed after a fall H as U₂ = √(U₁² + 2gH), and continuity (U₁ d₁² = U₂ d₂²) then gives d₂ = d₁[U₁²/(U₁² + 2gH)]^(1/4). The stream breaks up before the formula fails, as surface tension and air drag are neglected.

Diameter of a vertical circular jet after it has fallen a distance H from a section of diameter d₁ and speed U₁, from continuity and Bernoulli at atmospheric pressure, with no drag, break-up or surface tension.

Calculator

Solve for
m
m
0.0011
m/s
0.0550
m/s²
130
m
050
  • Speed after the fall, √(U₁² + 2gH)3.716 m/s
  • Diameter ratio, d₂/d₁0.7336
  • Area ratio, (d₂/d₁)²0.5382

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.

Jet diameter after the fall (m) current value 0.01467 m
d1Initial jet diameterKey driver
7.34e-40.734
U1Initial jet speed
0.002530.02
HFall height
0.005050.02
gGravitational acceleration
0.01170.0189
  • After 0.5 m of fall the 20 mm jet narrows to 14.67 mm, as its speed rises from 2 to 3.716 m/s.
  • The slower the jet starts, the stronger the narrowing: a jet leaving at near zero speed narrows rapidly over the first few centimetres.
Chart data as tables

Ranked variables

VariableTypical rangeLowest resultHighest resultSwing (m)Local stepChange in result
d1 Initial jet diameter0.001 to 1 m7.336e-40.73360.7329+10%+10 %
U1 Initial jet speed0.05 to 50 m/s0.0025270.019980.01745+10%+3.34 %
H Fall height0 to 50 m0.0050490.020.01495+10%−1.7 %
g Gravitational acceleration1 to 30 m/s²0.011710.018910.007202+10%−1.7 %

Sweep of Fall height

Fall height (m)Jet diameter after the fall (m)
00.02
6.250.008432
12.50.007118
18.750.006441
250.005998
31.250.005675
37.50.005423
43.750.005219
500.005049

Sweep one variable

Jet diameter after the fall (m)Hover, touch, or use the arrow keys on the chart
0.0050.010.0150.02 01020304050 Fall height (m) now 0.01467

Variables and how each one contributes

d2

Jet diameter after the fall

Result · m

What the equation gives you. Everything else feeds it.

d1

Initial jet diameter

m · typical 0.001 to 1

The initial jet diameter, in m. Raises the final diameter in direct proportion. Raising it by 10 % (to 0.022) moves the result by +10 %, from 0.01467 to 0.01614 m.

U1

Initial jet speed

m/s · typical 0.05 to 50

The initial jet speed, in m/s. A faster start means less speed-up relative to the start, so the jet narrows less. Raising it by 10 % (to 2.2) moves the result by +3.34 %, from 0.01467 to 0.01516 m.

g

Gravitational acceleration

m/s² · typical 1 to 30

The gravitational acceleration, in m/s². Stronger gravity speeds the jet more, so it narrows more. Raising it by 10 % (to 10.79) moves the result by −1.7 %, from 0.01467 to 0.01442 m.

H

Fall height

m · typical 0 to 50

The fall height, in m. A longer fall speeds the jet more, so it narrows more. Raising it by 10 % (to 0.55) moves the result by −1.7 %, from 0.01467 to 0.01442 m.

Worked example with the values above

  1. Speed after the fall: √(2² + 2 × 9.81 × 0.5) = 3.7162 m/s.
  2. Speed ratio U₁²/U₂² = 0.28965; fourth root = 0.73361.
  3. d₂ = 0.02 × 0.73361 = 0.014672 m.

Assumptions and limits

  • Steady, incompressible, inviscid flow outside the boundary layer, at atmospheric pressure where stated.
  • Uniform velocity profiles at the sections used.

Common mistakes

  • Using the area of the pipe where the jet area is needed.
  • Mixing gauge and absolute pressures in a force balance.
  • Forgetting that the force on the support is the reaction to the force on the fluid.

Statistics and uncertainty

Discharge and velocity coefficients vary with the Reynolds number and with the geometry, and measured jet distances carry the reading error of the ruler, so the results are no better than 2 % to 5 %.

Where it is used

  • Timing tank drainage and calibrating nozzles and orifices.
  • Sizing thrust blocks, deflectors and jet impact plates.

Maths you need

  • Torricelli’s law: jet speed √(2gh) from a head h
  • Momentum equation: force = rate of change of momentum
  • Continuity: Q = A U

Related formulas

Practise this formula