Bernoulli's Theorem Derivation- NCERT Guide
What Bernoulli's Theorem Actually Says
Bernoulli's theorem is about energy conservation in fluid flow. It states that for an incompressible, non-viscous fluid in steady flow, the sum of pressure energy, kinetic energy, and potential energy per unit volume remains constant along a streamline.
Mathematically, it looks like this:
P + ½ρv² + ρgh = constant
Where P is pressure, ρ is density, v is velocity, g is gravitational acceleration, and h is height. That's the equation you'll regurgitate in exams. But here's how it actually comes together.
The Assumptions You Can't Ignore
Before deriving anything, you need to know the constraints. Bernoulli's theorem doesn't work for everything. The derivation falls apart if these conditions aren't met.
- The fluid is incompressible — density stays constant.
- The flow is steady — velocity at any point doesn't change with time.
- The fluid is non-viscous — no internal friction, no energy loss to heat.
- The flow is irrotational or along a single streamline.
Break any of these, and the theorem becomes a rough approximation at best. Most real fluids are viscous, which is why Bernoulli's equation often gives you the wrong answer in practical engineering.
Setting Up the Problem
Picture a pipe with varying cross-section and height. Fluid enters at point A and exits at point B. At A, the cross-sectional area is A₁, velocity is v₁, pressure is P₁, and height is h₁. At B, those values are A₂, v₂, P₂, and h₂.
The fluid moves from A to B. We want to find how pressure, speed, and height relate to each other.
Mass and Volume Considerations
Because the fluid is incompressible, the volume flowing in at A equals the volume flowing out at B in the same time. This is the equation of continuity:
A₁v₁ = A₂v₂
Keep this in mind. It links the velocities to the pipe geometry.
The Work-Energy Approach
Here's where NCERT derives it. We apply the work-energy theorem to the fluid between A and B. The net work done on the fluid equals its change in kinetic energy.
But work comes from two sources in this setup:
- Work done by pressure forces at the inlet and outlet.
- Work done against gravity as the fluid changes height.
Let's calculate each.
Pressure Work at Inlet and Outlet
At point A, the fluid behind pushes the considered volume forward. Pressure P₁ acts over area A₁, moving the fluid through distance l₁.
Work done on the fluid at A:
W₁ = P₁A₁l₁
At point B, the fluid ahead resists. Pressure P₂ acts over area A₂, moving through distance l₂. This work is done by the fluid, so it's negative:
W₂ = –P₂A₂l₂
Net pressure work:
W_pressure = P₁A₁l₁ – P₂A₂l₂
But A₁l₁ and A₂l₂ are just volumes. And by continuity, the mass of fluid moved is the same, so the volume V is identical. Therefore:
W_pressure = (P₁ – P₂)V
Or per unit volume:
W_pressure = P₁ – P₂
Work Done Against Gravity
The fluid mass moved is m = ρV. It rises from height h₁ to h₂. The change in potential energy is:
ΔU = mg(h₂ – h₁) = ρVg(h₂ – h₁)
This is work done against gravity. Per unit volume:
W_gravity = ρg(h₂ – h₁)
Again, this is energy lost from the pressure-kinetic pool to lift the fluid.
Change in Kinetic Energy
The fluid speeds up or slows down between A and B. Change in kinetic energy:
ΔK = ½mv₂² – ½mv₁² = ½ρV(v₂² – v₁²)
Per unit volume:
ΔK = ½ρ(v₂² – v₁²)
Putting It All Together
Now apply work-energy. Net work equals change in kinetic energy:
W_pressure – W_gravity = ΔK
Substitute the per-volume expressions:
(P₁ – P₂) – ρg(h₂ – h₁) = ½ρ(v₂² – v₁²)
Rearrange. Move everything to one side:
P₁ + ½ρv₁² + ρgh₁ = P₂ + ½ρv₂² + ρgh₂
Since points A and B are arbitrary, the quantity P + ½ρv² + ρgh is constant along the streamline. That's Bernoulli's theorem.
Different Forms of the Equation
Depending on what you're solving for, you'll see this written differently. Here's the breakdown:
| Form | Equation | When to Use It |
|---|---|---|
| Pressure form | P + ½ρv² + ρgh = constant | General problems with varying height and speed |
| Head form | P/ρg + v²/2g + h = constant | Hydraulic engineering, comparing "heads" of energy |
| Energy per unit mass | P/ρ + v²/2 + gh = constant | Thermodynamics and compressible flow approximations |
| Horizontal flow | P + ½ρv² = constant | Pipes at constant height — speed up, pressure drops |
The "head form" is just dividing everything by ρg. Each term then has units of length. Engineers call them pressure head, velocity head, and elevation head. It looks cleaner on paper, but it's the same physics.
Where Students Screw This Up
Most derivation mistakes happen in these spots:
- Forgetting that P₂ does negative work because the fluid pushes outward against it.
- Mixing up the sign on gravity work — rising fluid loses available pressure energy.
- Assuming the theorem works for gases. It doesn't, unless density changes are negligible.
- Applying it across two different streamlines. The constant isn't the same for every streamline in rotational flow.
Also, NCERT problems often use the theorem for Toricelli's law (speed of efflux) or the venturi meter. In both cases, the derivation above is the starting point. Don't memorize the end formulas. Start from P + ½ρv² + ρgh = constant and derive the specific case every time.
Quick Derivation Check: Horizontal Pipe
Let's test it. A horizontal pipe narrows from area A₁ to A₂. Height is constant, so h₁ = h₂.
Bernoulli's equation reduces to:
P₁ + ½ρv₁² = P₂ + ½ρv₂²
From continuity, A₁v₁ = A₂v₂. If A₂ < A₁, then v₂ > v₁.
Substitute back:
P₁ – P₂ = ½ρ(v₂² – v₁²) > 0
So P₂ < P₁. The fluid speeds up where the pipe narrows, and pressure drops. This is the venturi effect. It's not magic. It's just energy shuffling from pressure to kinetic.
Limitations You Need to Know
Bernoulli's theorem is textbook idealization. Real life is messier.
- Viscosity causes energy loss. The theorem ignores it. For long pipes, you need the Hagen-Poiseuille equation or Darcy-Weisbach instead.
- Turbulence destroys streamline flow. The theorem assumes laminar, orderly motion.
- Compressibility matters for gases at high speeds. Airflow over airplane wings at subsonic speeds is fine, but near Mach 1, this breaks down.
- Heat transfer and external work (like pumps) aren't included. This is conservation of mechanical energy only.
If your fluid is water moving slowly through a short pipe, Bernoulli works great. If it's blood in arteries or air in a jet engine, you need heavier tools.
Getting Started: Solving NCERT Problems
Here's the blunt workflow for typical exam problems:
- Draw the diagram. Mark two points — usually where you know the most data and where you want to find something.
- Check if Bernoulli applies. Is the fluid incompressible? Non-viscous? Steady flow? If yes, proceed.
- Write the full equation: P₁ + ½ρv₁² + ρgh₁ = P₂ + ½ρv₂² + ρgh₂.
- Use continuity if you have pipe areas: A₁v₁ = A₂v₂.
- Plug in what you know. Solve for the unknown. Watch your units — Pascals for pressure, m/s for velocity, meters for height.
- If one point is open to atmosphere, P = P_atm ≈ 10⁵ Pa.
- If a tank is large, surface velocity is approximately zero. Use v₁ ≈ 0.
That's it. No shortcuts. No intuition needed. Just algebra and attention to signs.
The Bottom Line
Bernoulli's theorem derives cleanly from the work-energy theorem applied to a fluid element. Pressure does work. Gravity steals energy. What's left shows up as kinetic energy. The equation P + ½ρv² + ρgh = constant is just bookkeeping.
It won't solve every fluid problem. It's a simplification. But for NCERT, it's enough. Learn the derivation once, practice the algebra ten times, and stop overthinking it. The math is straightforward. Your mistakes will be sign errors and unit conversions, not conceptual gaps.