Conservation Laws
Mass, momentum, and energy - the fundamental equations of fluid motion
Introduction
The motion of fluids is governed by conservation laws - mass, momentum, and energy cannot be created or destroyed, only transported and converted. These fundamental principles, combined with constitutive relations, give us the complete equations of fluid dynamics.
We present both integral forms (useful for control volume analysis) and differential forms (useful for detailed flow field solutions).
Conservation of Mass (Continuity)
Integral Form
The rate of change of mass in a control volume equals the net mass flux through the surface:
For steady flow: ∮ρ(v·n)dA = 0 → Mass in = Mass out
Differential Form
Using the divergence theorem:
Or equivalently, using the material derivative:
Incompressible Flow
When Dρ/Dt = 0 (density of a fluid particle doesn't change), continuity simplifies to:
Valid for liquids and low-speed (Ma < 0.3) gas flows.
Conservation of Momentum
Integral Form (Control Volume)
Newton's second law applied to a control volume:
Forces include pressure, gravity, viscous stresses, and external forces.
Cauchy Momentum Equation
General differential form (valid for any continuous medium):
where τ is the deviatoric stress tensor (viscous stresses for Newtonian fluids).
Navier-Stokes Equations
For incompressible Newtonian fluids with constant viscosity:
∂v/∂t
Unsteady
(v·∇)v
Convection
μ∇²v
Diffusion
-∇p + ρg
Pressure + Gravity
Euler Equations (Inviscid)
When viscous effects are negligible (high Re, away from boundaries):
Conservation of Energy
First Law for a Control Volume
Energy balance including work and heat transfer:
where e = u + v²/2 + gz is specific energy (internal + kinetic + potential)
Differential Energy Equation
For a compressible fluid:
Terms: heat conduction, pressure work, viscous dissipation
For Incompressible Flow
Often temperature can be treated separately from mechanics (weak coupling), and the energy equation simplifies to tracking temperature evolution via heat conduction and advection.
Bernoulli Equation
A special case of energy/momentum conservation for steady, inviscid, incompressible flow along a streamline:
p
Static pressure
½ρv²
Dynamic pressure
ρgz
Hydrostatic pressure
Extended Forms
Unsteady Bernoulli
With Head Loss (Engineering)
hL accounts for viscous losses (friction, minor losses)
Applications
Pitot Tube
Velocity from Bernoulli: v = √(2(p₀-p)/ρ) where p₀ is stagnation pressure
Venturi Meter
Flow rate from pressure difference using continuity + Bernoulli
Siphon
Flow driven by elevation difference - must stay above vapor pressure
Jet Propulsion
Momentum flux from nozzle provides thrust: F = ṁ(vexit - vinlet)