Bernoulli’s Equation
Bernoulli’s equation is one of the most important equations in fluid mechanics. It expresses the conservation of energy along a streamline for steady, incompressible, inviscid flow:
P/ρg + V²/2g + z = constant
Or equivalently:
P₁/ρg + V₁²/2g + z₁ = P₂/ρg + V₂²/2g + z₂
Where:
- P = static pressure (Pa)
- ρ = fluid density (kg/m³)
- g = gravitational acceleration (9.81 m/s²)
- V = fluid velocity (m/s)
- z = elevation above datum (m)
Each term represents a head (pressure head + velocity head + elevation head = total head = constant).
Derivation from Work-Energy Theorem
Bernoulli’s equation can be derived by applying Newton’s second law (F = ma) along a streamline to a fluid element, or by applying the first law of thermodynamics to a control volume of inviscid, steady, incompressible flow. Key steps:
- Consider a fluid element of mass dm moving along a streamline
- Forces acting: pressure forces on both faces + component of gravity
- Apply F = ma along the streamline (Euler’s equation)
- Integrate Euler’s equation along the streamline
- Result: P + ½ρV² + ρgz = constant
Assumptions of Bernoulli’s Equation
- Steady flow — fluid properties at any point do not change with time
- Incompressible flow — constant fluid density (valid for liquids; gases below Mach 0.3)
- Inviscid flow — no viscous (frictional) effects (no energy loss)
- Along a streamline — the equation applies between two points on the same streamline
- No work or heat transfer between the two points considered
Applications of Bernoulli’s Equation
| Application | How Bernoulli’s is Used |
|---|---|
| Venturi meter | Pressure difference between throat and inlet gives flow velocity |
| Pitot tube | Stagnation pressure minus static pressure gives velocity |
| Orifice plate | Flow rate from upstream and throat pressures |
| Aerofoil / aircraft lift | Higher velocity over the upper surface → lower pressure → lift |
| Carburetor | High-velocity air in venturi creates low pressure, draws fuel |
| Siphon | Negative gauge pressure at the top of the siphon drives flow |
Limitations of Bernoulli’s Equation
- Not valid for viscous flow — ignores friction losses (pipe flow needs the Darcy-Weisbach equation)
- Not valid for compressible flow at high Mach numbers
- Not valid across turbomachinery (pumps, fans, turbines) — work is added or extracted
- Not valid across shock waves
- Only along a streamline — different streamlines can have different Bernoulli constants unless flow is irrotational
Modified Bernoulli’s Equation (with Head Loss)
For real fluid flow with friction losses and/or pump work:
P₁/ρg + V₁²/2g + z₁ + h_pump = P₂/ρg + V₂²/2g + z₂ + h_L
Where h_pump = energy added by pump per unit weight, and h_L = head loss due to friction and minor losses.
Lab Experiment
The Bernoulli’s Theorem Apparatus consists of a convergent-divergent section with pressure tappings at multiple points. Students:
- Set a steady flow rate through the apparatus
- Read the piezometric (static) head at each tapping using a manometer bank
- Measure the flow velocity using a rotameter or by timing collection
- Calculate the total head at each tapping and verify it is constant (Bernoulli’s theorem)
- Observe how static pressure decreases and velocity increases at the throat
Contact Scientico India for CE-certified Bernoulli’s Theorem Apparatus for your fluid mechanics lab.
Scientico India manufactures this and the full range of Fluid Mechanics Lab equipment — CE-certified and supplied to engineering colleges worldwide.
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