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SCIENCE · INVESTIGATE AND EXPLAIN

Account for pressure work in ideal flow

Use Bernoulli’s equation to explain pressure changes along an accelerating liquid stream.

Learning outcome: Apply a horizontal ideal-flow energy balance, distinguish gauge and absolute pressure, and verify that pressure work supplies the change in kinetic-energy flow.

Starting recap

Pressure differences can do work on a moving volume. Energy per volume has the same units as pressure.

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Try

Fluid moves faster in the narrow section. What supplies its extra kinetic energy when there is no pump between the sections?

Open the experiment

Predict

At 4 L/s and outlet area 20 cm², predict the pressure change from the 120 kPa inlet and compare the pressure-work and kinetic-energy rates.

Experiment

Compare outlet areas 20 and 10 cm² at fixed flow. Then test 8 L/s at 10 cm² and interpret negative gauge pressure. Compare the two total mechanical energy-flow entries and test equal areas.

Conserve flow through a changing cross-section

Worked teaching model · synthetic values · Steady incompressible ideal liquid of density 1000 kg/m³ in a horizontal pipe with inlet area 40 cm² and inlet absolute pressure 120 kPa. A supply maintains the chosen flow; downstream pressure adjusts to the calculated value. Uniform section speeds approximate the ideal flow. No branches, leakage, storage, pump or turbine between sections, viscosity or turbulent losses. The outlet is a section of a pressurized pipe, not necessarily an opening to atmosphere. Gauge reference is 100 kPa. No transient, cavitation or real-pipe sizing prediction.

Reset keeps your prediction, captures and practice history.

Area changes speed at fixed flow · equal elevation at both sectionsInlet 40 cm² · 1.000 m/sOutlet 20 cm² · 2.000 m/sDrawn diameter scales with √area; no particle travel time or pipe length is inferred.
Section speeds (m/s) · same volume flow at both sections02468Inlet: 1.000Outlet: 2.000
Equal mass flow and mechanical energy flow
SectionArea (cm²)Speed (m/s)Flow (L/s)Mass flow (kg/s)Absolute pressure (kPa)Gauge pressure (kPa)Pressure work rate (W)Kinetic energy flow (W)Sum (W)
Inlet40.01.0004.0004.000120.00020.000480.0002.000482.000
Outlet20.02.0004.0004.000118.50018.500474.0008.000482.000

Pressure work entering minus pressure work leaving is 6.000 W. Kinetic-energy flow increases by 6.000 W. These are mechanical rates at the sections, not measured electrical pump consumption.

Inlet speed 1.000 m/s; outlet speed 2.000 m/s. Both carry 4.000 L/s and 4.000 kg/s.

Outlet pressure 118.500 kPa absolute (18.500 kPa gauge). Pressure drop 1.500 kPa supplies 6.000 W of net pressure work, matching the kinetic-energy flow increase. The downstream boundary must support this pressure.

Captures preserve recipes and replay their calculated results. They are synthetic model evidence, not physical measurements.

Understand

Identify the work that accelerates the liquid

Continuity predicts a higher speed in a narrower section at fixed incompressible flow. It does not by itself explain where the increased kinetic energy comes from. A pressure difference can do net work on the moving liquid.

The inlet in this model is held at 120 kPa absolute pressure. A supply maintains the selected flow rate. The outlet is a downstream section of a pressurized pipe, not necessarily an opening to the atmosphere. Its pressure is calculated from the ideal energy balance and must be compatible with the downstream system. The model does not simultaneously prescribe an unrelated outlet pressure.

Write an energy account per volume

For steady incompressible ideal flow along the modeled stream, p + ½ρv² + ρgz remains constant when there is no intervening pump, turbine or dissipative loss. p is pressure in Pa, ρ is density in kg/m³, v is speed in m/s, g is gravitational acceleration and z is elevation in metres. Each term has units of energy per volume, J/m³, equivalent to Pa.

The two sections here have equal elevation, so their gravitational terms cancel. The relation becomes p₂ = p₁ + ½ρ(v₁² − v₂²). If the downstream speed is greater under these conditions, its pressure is smaller. The OpenStax Bernoulli reference connects this relation to pressure work and mechanical-energy change.

This is a comparison along one ideal flow with stated boundary conditions. It is not a universal rule that any faster-moving fluid anywhere must have lower pressure than any slower fluid. Different streamlines, pumps, heights, losses or transient conditions can invalidate that comparison.

Work through the default case

At flow 4 L/s, the 40 cm² inlet speed is 1 m/s. For a 20 cm² outlet, speed is 2 m/s. The increase in kinetic energy per volume is ½ × 1000 × (2² − 1²) = 1500 Pa, or 1.5 kPa.

Outlet absolute pressure is therefore 120 − 1.5 = 118.5 kPa. Relative to the 100 kPa gauge reference, this is 18.5 kPa gauge. The inlet gauge pressure is 20 kPa. Either consistent pressure reference gives the same 1.5 kPa difference.

Capture this case and compare it with an outlet area of 10 cm² at the same 4 L/s. Outlet speed becomes 4 m/s and the pressure drop becomes ½ × 1000 × (16 − 1) = 7500 Pa, or 7.5 kPa. Outlet absolute pressure is 112.5 kPa. The squared-speed term makes the pressure change nonlinear in flow speed.

Check the power ledger independently

A pressure p acting through volume flow Q has pressure-work rate pQ, measured in watts. Kinetic energy transported per second is ½ρQv² under the model’s uniform-speed assumption. A nonuniform real velocity profile requires a corresponding energy-flow correction.

For the default case, inlet pressure work is 120000 × 0.004 = 480 W. Outlet pressure work leaving is 118500 × 0.004 = 474 W. Their difference is 6 W of net pressure work on the fluid between sections.

Kinetic-energy flow is ½ × 1000 × 0.004 × 1² = 2 W at the inlet and 8 W at the outlet. Its increase is also 6 W. The sum of pressure-work and kinetic-energy rates is 482 W at each section. The equal totals check the ideal mechanical account; they are not a measurement of electrical pump consumption.

Changing both pressure references by the same constant shifts the two pressure-work entries equally because Q is the same. Their difference remains unchanged. Keep one reference throughout rather than mixing an absolute inlet reading with a gauge outlet reading.

Interpret negative gauge pressure correctly

Set flow to 8 L/s and outlet area to 10 cm². Speeds are 2 and 8 m/s. The pressure drop is ½ × 1000 × (64 − 4) = 30 kPa. Outlet pressure is 90 kPa absolute, or −10 kPa gauge relative to 100 kPa.

Negative gauge pressure means below the reference pressure, not negative absolute pressure. The modeled absolute pressure remains positive. Applying this result to a real liquid would also require checking its vapor pressure, the downstream boundary and whether the ideal assumptions remain credible. The widget does not model cavitation or select a real pipe design.

At equal areas the speeds match and the ideal pressure drop is zero. A real pipe can still require a pressure drop to overcome viscous losses. At zero flow, both pressure-work rates and kinetic-energy rates vanish, while the equal absolute pressures remain 120 kPa.

Transfer to changed speeds

An ideal horizontal stream of density 800 kg/m³ accelerates from 2 to 5 m/s. Inlet absolute pressure is 150 kPa. Find outlet absolute pressure. If volume flow is 0.003 m³/s, calculate net pressure-work rate and check it against the change in kinetic-energy flow.

Check the Bernoulli transfer

The kinetic-energy increase per volume is ½ × 800 × (25 − 4) = 8400 Pa = 8.4 kPa. Outlet absolute pressure is 141.6 kPa. Net pressure-work rate is 8400 × 0.003 = 25.2 W. Kinetic-energy flow rises from ½ × 800 × 0.003 × 4 = 4.8 W to 30 W, also an increase of 25.2 W. Equal elevation and no losses or shaft work are essential to this result.

Apply

A horizontal ideal liquid of density 1000 kg/m³ accelerates from 1 to 2 m/s. Inlet absolute pressure is 120 kPa. Outlet absolute pressure is:

Public practice checks a specific claim. It does not establish independent mastery.

Explain the energy source for increased speed, identify the prescribed boundary conditions, and state why faster flow is not a universal guarantee of lower pressure in unrelated streams.

Continue

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