Fluid Dynamics and Bernoulli's Equation
Key Takeaways
- Continuity equation (conservation of mass): A₁V₁ = A₂V₂ for incompressible flow in a pipe.
- Bernoulli's equation: P₁/γ + V₁²/2g + z₁ = P₂/γ + V₂²/2g + z₂ (along a streamline, inviscid, incompressible, steady).
- Reynolds number Re = ρVD/μ = VD/ν determines flow regime: Re < 2,300 laminar, Re > 4,000 turbulent.
- The energy equation adds head losses: P₁/γ + V₁²/2g + z₁ = P₂/γ + V₂²/2g + z₂ + hL.
- Head loss includes major losses (pipe friction: hf = fLV²/(2gD)) and minor losses (fittings: hm = KV²/(2g)).
- The Darcy friction factor f comes from the Moody diagram (function of Re and relative roughness ε/D).
Fluid Dynamics and Bernoulli's Equation
Conservation of Mass (Continuity)
For steady, incompressible flow:
where Q = volumetric flow rate (m³/s).
Mass flow rate: ṁ = ρAV = ρQ (kg/s)
Bernoulli's Equation
For steady, inviscid, incompressible flow along a streamline:
Each term has units of length (head):
- P/γ = pressure head
- V²/2g = velocity head
- z = elevation head
Total head (Bernoulli constant) = P/γ + V²/2g + z = constant along a streamline
Applications of Bernoulli's Equation
Pitot Tube: Measures velocity from stagnation pressure
Venturi Meter: Measures flow rate from pressure difference at a constriction
Free Jet: Velocity of fluid exiting a tank
(Torricelli's theorem — same as free-fall velocity from height h)
Reynolds Number
| Re Range | Flow Regime |
|---|---|
| Re < 2,300 | Laminar |
| 2,300 < Re < 4,000 | Transitional |
| Re > 4,000 | Turbulent |
Dimensionless Numbers Summary
| Number | Formula | Physical Meaning |
|---|---|---|
| Reynolds (Re) | ρVL/μ | Inertia / Viscous forces |
| Froude (Fr) | V/√(gL) | Inertia / Gravity forces |
| Mach (Ma) | V/c | Flow velocity / Speed of sound |
Pipe Flow and Head Losses
The Energy Equation (Modified Bernoulli)
where hL = total head loss = major losses + minor losses.
Major Losses (Pipe Friction) — Darcy-Weisbach Equation
where f = Darcy friction factor (from Moody diagram or Colebrook equation).
For laminar flow (Re < 2,300):
For turbulent flow: Use the Moody diagram with Re and relative roughness ε/D.
Minor Losses (Fittings, Valves, Etc.)
| Fitting | K (typical) |
|---|---|
| 90° elbow | 0.3-1.5 |
| 45° elbow | 0.2-0.4 |
| Tee (branch) | 1.0-2.0 |
| Gate valve (fully open) | 0.2 |
| Globe valve (fully open) | 6-10 |
| Entrance (sharp) | 0.5 |
| Entrance (rounded) | 0.03-0.1 |
| Exit | 1.0 |
| Sudden expansion | (1 - A₁/A₂)² |
| Sudden contraction | 0.5(1 - A₂/A₁) |
Open-Channel Flow
Manning's Equation
where:
- n = Manning's roughness coefficient
- Rh = hydraulic radius = A/P (area/wetted perimeter)
- S = slope of the energy grade line
Froude Number
| Fr | Flow Type |
|---|---|
| Fr < 1 | Subcritical (deep, slow) |
| Fr = 1 | Critical |
| Fr > 1 | Supercritical (shallow, fast) |
Water flows through a pipe that narrows from 10 cm diameter to 5 cm diameter. If the velocity at the larger section is 2 m/s, what is the velocity at the smaller section?
Water exits a tank through a hole 5 m below the water surface. What is the exit velocity? (Assume Torricelli's theorem applies)
Water flows in a 0.1 m diameter pipe at 1.5 m/s. If ν = 10⁻⁶ m²/s, the Reynolds number is:
For fully developed laminar flow in a pipe, the Darcy friction factor is: