Bernoulli's equation
Along a streamline in steady, frictionless flow, pressure, kinetic energy and height trade off against each other, but their sum stays fixed:
p + ½ρv² + ρgh = C
- p
- pressure
- Pa
- ρ
- density
- kg/m³
- v
- flow speed
- m/s
- g
- gravitational acceleration
- m/s²
- h
- height above a datum
- m
- C
- constant along the streamline
- Pa
- D
- pipe diameter
- m
- Δh
- rise from inlet to outlet
- m
- H
- total head
- m
| v2 = v1(D1/D2)² | 5.56 m/s |
| ½ρ(v1² − v2²) | −13.4 kPa |
| −ρg Δh | −19.6 kPa |
| p2 | 167 kPa |
Worked example
Uses the values in Fig. 1.2-1. Change them and the working updates.
Given
- p1inlet gauge pressure200 kPa
- v1inlet speed2 m/s
- D1inlet diameter100 mm
- D2outlet diameter60 mm
- Δhoutlet height above inlet2 m
- ρwater998 kg/m³
Find
The gauge pressure p2 at the outlet.
Solution
v2 = v1(D1/D2)² = 2 m/s × (100/60)² = 5.56 m/s
p2 = p1 + ½ρ(v1² − v2²) − ρg Δh
= 200 kPa + ½ × 998 kg/m³ × ((2 m/s)² − (5.56 m/s)²) − 998 kg/m³ × 9.81 m/s² × 2 m
= 200 − 13.4 − 19.6 = 167 kPa
Answer
p2 = 167 kPa
That is gauge pressure, about 268 kPa absolute.
Related forms
-
Draining tank (Torricelli)
v = √(2gh)
-
Pitot tube
v = √(2Δpρ)
-
Head form, in metres
pρg + v²2g + z = H
Assumptions
- Flow is steady and incompressible.
- There is no friction. Real pipes lose head to friction, so the real outlet pressure is lower.
- The equation applies along one streamline, or between sections where the flow is uniform.
- No pump or turbine sits between the two points.
- Pressures here are gauge. Absolute pressure is gauge plus about 101.3 kPa, and water starts to boil (cavitate) near 2.3 kPa absolute at 20 °C.
Derivation
Follow a small volume V of fluid from section 1 to section 2.
- The pressure difference does work on it:
(p1 − p2)V. - Its kinetic energy rises by
½ρV(v2² − v1²), and its potential energy byρVg(h2 − h1). - With no friction, work in equals energy gained. Divide by V and collect each section's terms:
p1 + ½ρv1² + ρgh1 = p2 + ½ρv2² + ρgh2.