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).
Last updated: March 2026

Fluid Dynamics and Bernoulli's Equation

Conservation of Mass (Continuity)

For steady, incompressible flow: A1V1=A2V2=QA_1 V_1 = A_2 V_2 = Q

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:

P1γ+V122g+z1=P2γ+V222g+z2\frac{P_1}{\gamma} + \frac{V_1^2}{2g} + z_1 = \frac{P_2}{\gamma} + \frac{V_2^2}{2g} + z_2

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 V=2(PstagPstatic)ρV = \sqrt{\frac{2(P_{stag} - P_{static})}{\rho}}

Venturi Meter: Measures flow rate from pressure difference at a constriction Q=CdA22g(h1h2)1(A2/A1)2Q = C_d A_2 \sqrt{\frac{2g(h_1 - h_2)}{1 - (A_2/A_1)^2}}

Free Jet: Velocity of fluid exiting a tank V=2ghV = \sqrt{2gh}

(Torricelli's theorem — same as free-fall velocity from height h)

Reynolds Number

Re=ρVDμ=VDνRe = \frac{\rho V D}{\mu} = \frac{VD}{\nu}

Re RangeFlow Regime
Re < 2,300Laminar
2,300 < Re < 4,000Transitional
Re > 4,000Turbulent

Dimensionless Numbers Summary

NumberFormulaPhysical Meaning
Reynolds (Re)ρVL/μInertia / Viscous forces
Froude (Fr)V/√(gL)Inertia / Gravity forces
Mach (Ma)V/cFlow velocity / Speed of sound

Pipe Flow and Head Losses

The Energy Equation (Modified Bernoulli)

P1γ+V122g+z1=P2γ+V222g+z2+hL\frac{P_1}{\gamma} + \frac{V_1^2}{2g} + z_1 = \frac{P_2}{\gamma} + \frac{V_2^2}{2g} + z_2 + h_L

where hL = total head loss = major losses + minor losses.

Major Losses (Pipe Friction) — Darcy-Weisbach Equation

hf=fLDV22gh_f = f \frac{L}{D} \frac{V^2}{2g}

where f = Darcy friction factor (from Moody diagram or Colebrook equation).

For laminar flow (Re < 2,300): f=64Ref = \frac{64}{Re}

For turbulent flow: Use the Moody diagram with Re and relative roughness ε/D.

Minor Losses (Fittings, Valves, Etc.)

hm=KV22gh_m = K \frac{V^2}{2g}

FittingK (typical)
90° elbow0.3-1.5
45° elbow0.2-0.4
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
Exit1.0
Sudden expansion(1 - A₁/A₂)²
Sudden contraction0.5(1 - A₂/A₁)

Open-Channel Flow

Manning's Equation

V=1nRh2/3S1/2(SI units)V = \frac{1}{n} R_h^{2/3} S^{1/2} \quad (\text{SI units})

where:

  • n = Manning's roughness coefficient
  • Rh = hydraulic radius = A/P (area/wetted perimeter)
  • S = slope of the energy grade line

Froude Number

Fr=VgDhFr = \frac{V}{\sqrt{gD_h}}

FrFlow Type
Fr < 1Subcritical (deep, slow)
Fr = 1Critical
Fr > 1Supercritical (shallow, fast)
Test Your Knowledge

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?

A
B
C
D
Test Your Knowledge

Water exits a tank through a hole 5 m below the water surface. What is the exit velocity? (Assume Torricelli's theorem applies)

A
B
C
D
Test Your Knowledge

Water flows in a 0.1 m diameter pipe at 1.5 m/s. If ν = 10⁻⁶ m²/s, the Reynolds number is:

A
B
C
D
Test Your Knowledge

For fully developed laminar flow in a pipe, the Darcy friction factor is:

A
B
C
D