Fluid Dynamics: Energy & Momentum

Learning Objectives

  • Understand the fundamental laws of fluid dynamics including conservation of mass, energy, and momentum.
  • Apply Euler's and Bernoulli's equations to fluid flow problems.
  • Analyze pressure, velocity, and elevation heads in steady flow.
  • Understand the role of the Navier-Stokes equations in viscous flow.
  • Calculate flow velocities and discharge using Torricelli's Theorem, Venturi meters, and Pitot tubes.
  • Apply the impulse-momentum principle to calculate forces on fluid boundaries, including stationary and moving vanes.

Dynamics of fluid flow including Bernoulli's equation, energy lines, the impulse-momentum principle, and practical applications.

Overview

Fluid dynamics considers the forces causing fluid motion in hydraulic systems, such as flow through pipes, channels, and pumps. The analysis relies on three fundamental laws of physics applied to fluid mechanics.

Conservation of Mass (Continuity Equation)

The principle that mass can neither be created nor destroyed. For steady, incompressible flow, the volumetric flow rate into a system equals the volumetric flow rate out (Qin=QoutQ_{in} = Q_{out}).

Conservation of Energy (Bernoulli's Equation)

The principle that energy cannot be created or destroyed, only transformed. In fluid dynamics, this relates the pressure, kinetic, and potential energy of a fluid.

Conservation of Momentum (Impulse-Momentum Principle)

Based on Newton's Second Law, this principle states that the net force on a fluid mass equals its rate of change of momentum. It is crucial for calculating forces on pipe bends and turbine blades.

Euler's Equation of Motion

Euler's equation is the fundamental differential equation describing the motion of an inviscid (frictionless) fluid. It forms the basis for deriving Bernoulli's equation.

Euler's Equation

Applying Newton's Second Law to an infinitesimal fluid particle along a streamline, assuming zero viscosity (inviscid flow), yields Euler's equation of motion.

Euler's Equation

The differential equation describing the motion of an inviscid fluid along a streamline.

dPฯ+VdV+gdz=0\frac{dP}{\rho} + V dV + g dz = 0

Variables

SymbolDescriptionUnit
PPPressurePa
Fluid densitykg/m3kg/m^3
VVFlow velocitym/s
ggAcceleration due to gravitym/s2m/s^2
zzElevationm

Euler to Bernoulli Integration

Integrating Euler's equation for steady, incompressible flow yields the well-known Bernoulli's Equation.

Concept Overview

Bernoulli's equation relates pressure, velocity, and elevation for an inviscid, incompressible fluid in steady flow along a streamline. It states that the total mechanical energy per unit weight (head) remains constant.

Bernoulli's Equation

The mathematical statement of the conservation of mechanical energy for steady, incompressible, frictionless flow along a streamline.

P1ฮณ+V122g+z1=P2ฮณ+V222g+z2=H\frac{P_1}{\gamma} + \frac{V_1^2}{2g} + z_1 = \frac{P_2}{\gamma} + \frac{V_2^2}{2g} + z_2 = H

Variables

SymbolDescriptionUnit
PPPressurePa
Specific weight of the fluidN/m3N/m^3
VVFlow velocitym/s
ggAcceleration due to gravitym/s2m/s^2
zzElevation above datumm
HHTotal head (constant along streamline)m

Bernoulli Head Components

The components of Bernoulli's equation represent distinct forms of energy per unit weight:

  • Pressure Head: P/ฮณP/\gamma (Work done by pressure forces)
  • Velocity Head: V2/2gV^2/2g (Kinetic Energy)
  • Elevation Head: zz (Potential Energy)
  • Total Head (HH): Sum of the three components.

Restrictions for Bernoulli's Equation

Restrictions for applying Bernoulli's Equation:

  • Steady flow: Flow conditions (velocity, pressure) do not change with time at any given point.
  • Incompressible flow: Fluid density (ฯ\rho) remains constant (generally valid for water and other liquids).
  • Frictionless flow (Inviscid): Internal fluid friction and friction against boundaries are neglected.
  • Along a streamline: The points being analyzed must lie on the same continuous path of fluid particles.

Interactive Simulation

Use the interactive Venturi Meter simulation below to visualize how pressure changes as velocity changes due to varying cross-sectional area. Observe the trade-off between kinetic energy and pressure energy.

Bernoulli's Principle (Venturi Meter)

V1V2P1P2
Inlet (1)
150.0 kPa
2.00 m/s
Throat (2)
0.0 kPa
0.00 m/s

As the area decreases at the throat, velocity must increase (Continuity). This increase in kinetic energy causes a drop in pressure potential energy (Bernoulli). If pressure drops below vapor pressure, cavitation occurs.

Graphical Representation of Head

The Energy Line and Hydraulic Grade Line provide a graphical representation of the energy state along a fluid flow path.

  • Energy Line (EL): Represents the total head (HH). In ideal flow, EL is horizontal. In real flow, EL slopes downward due to friction loss (hfh_f).
  • Hydraulic Grade Line (HGL): Represents the sum of pressure and elevation heads (piezometric head). The HGL is always below the EL by the velocity head (V2/2gV^2/2g).

Energy Line (EL)

Calculates the total head at any point along the streamline.

EL=Pฮณ+V22g+zEL = \frac{P}{\gamma} + \frac{V^2}{2g} + z

Variables

SymbolDescriptionUnit
ELELEnergy Line (total head)m
PPPressurePa
Specific weight of fluidN/m3N/m^3
VVFlow velocitym/s
ggAcceleration due to gravitym/s2m/s^2
zzElevation above datumm

Hydraulic Grade Line (HGL)

Calculates the piezometric head, representing the height to which liquid would rise in a piezometer tube.

HGL=Pฮณ+zHGL = \frac{P}{\gamma} + z

Variables

SymbolDescriptionUnit
HGLHGLHydraulic Grade Linem
PPPressurePa
Specific weight of fluidN/m3N/m^3
zzElevation above datumm

Viscous Flow Overview

While Bernoulli's Equation assumes inviscid (frictionless) flow, the Navier-Stokes Equations describe the motion of real, viscous fluid substances. They are derived from the conservation of momentum (Newton's second law) applied to a fluid particle, adding terms for internal viscous stresses.

Navier-Stokes Equations

These non-linear partial differential equations represent the balance between inertial, pressure, viscous, and body forces in a fluid. They are the fundamental equations of fluid dynamics.

Navier-Stokes Equations

The vector representation of the conservation of momentum for incompressible Newtonian viscous flow.

ฯ(โˆ‚Vโƒ—โˆ‚t+Vโƒ—โ‹…โˆ‡Vโƒ—)=โˆ’โˆ‡P+ฮผโˆ‡2Vโƒ—+ฯgโƒ—\rho \left(\frac{\partial \vec{V}}{\partial t} + \vec{V} \cdot \nabla \vec{V}\right) = -\nabla P + \mu \nabla^2 \vec{V} + \rho \vec{g}

Variables

SymbolDescriptionUnit
Fluid densitykg/m3kg/m^3
Velocity vectorm/s
ttTimes
PPPressurePa
Dynamic viscosityPaยทs
Gravitational acceleration vectorm/s2m/s^2

Navier-Stokes Force Terms

The terms in the Navier-Stokes equations represent distinct physical forces acting on the fluid volume:

  • Inertial Forces (left-hand side): Includes local acceleration โˆ‚Vโƒ—/โˆ‚t\partial \vec{V} / \partial t (changes over time) and convective acceleration Vโƒ—โ‹…โˆ‡Vโƒ—\vec{V} \cdot \nabla \vec{V} (changes over space).
  • Pressure Forces (โˆ’โˆ‡P-\nabla P): Forces arising due to the pressure gradient across the fluid.
  • Viscous Forces (ฮผโˆ‡2Vโƒ—\mu \nabla^2 \vec{V}): Forces arising from fluid shear stress and internal friction (viscosity).
  • Body Forces (ฯgโƒ—\rho \vec{g}): External forces acting on the entire bulk of the fluid, primarily gravity in civil engineering applications.

Analytical Challenges of Navier-Stokes Equations

Solving the Navier-Stokes equations analytically is one of the biggest challenges in mathematics and physics (a Millennium Prize Problem). They are typically solved numerically using Computational Fluid Dynamics (CFD).

Applications of Bernoulli's Equation

Bernoulli's equation supports common velocity and flow measurement tools such as orifices, Venturi meters, and Pitot tubes.

Torricelli's Theorem

The principle stating that the velocity of efflux of a fluid from an orifice under gravity is equivalent to the velocity acquired by a body falling freely from rest through the same height.

Torricelli's Theorem

Calculates the theoretical velocity of a liquid exiting an orifice.

V=2ghV = \sqrt{2gh}

Variables

SymbolDescriptionUnit
VVVelocity of effluxm/s
ggAcceleration due to gravitym/s2m/s^2
hhDepth of fluid above the orificem

Venturi Meter

A flow measurement device consisting of a converging section, a throat, and a diverging section. It uses the pressure difference between the inlet and the throat to determine volumetric flow rate.

Venturi Meter Discharge

Calculates the flow rate (discharge) through a Venturi meter based on pressure differential.

Q=CdA1A22g(h1โˆ’h2)A12โˆ’A22Q = C_d A_1 A_2 \sqrt{\frac{2g(h_1-h_2)}{A_1^2 - A_2^2}}

Variables

SymbolDescriptionUnit
QQVolumetric flow rate (discharge)m3/sm^3/s
CdC_dCoefficient of discharge (typically 0.96 - 0.99)dimensionless
A1A_1Cross-sectional area of inlet pipem2m^2
A2A_2Cross-sectional area of throatm2m^2
ggAcceleration due to gravitym/s2m/s^2
h1h_1Piezometric head at inletm
h2h_2Piezometric head at throatm

Pitot Tube

An instrument used to measure the local flow velocity at a specific point in a fluid stream by converting kinetic energy into pressure energy at a stagnation point.

Pitot Tube Velocity

Calculates point velocity using the difference between stagnation and static pressures.

V=2gฮ”hV = \sqrt{2g \Delta h}

Variables

SymbolDescriptionUnit
VVLocal velocitym/s
ggAcceleration due to gravitym/s2m/s^2
Difference between total (stagnation) head and static headm

Example Application: Determining Flow Velocity using Pitot Tube

Suppose a Pitot tube is placed in a river and the difference between stagnation and static pressure heads is measured to be 0.15 m. Using the Pitot Tube Velocity formula:

V=2(9.81ย m/s2)(0.15ย m)โ‰ˆ1.71ย m/sV = \sqrt{2(9.81\text{ m/s}^2)(0.15\text{ m})} \approx 1.71\text{ m/s}

This real-world application shows how static and dynamic heads combine to offer a direct measurement of fluid velocity.

Incompressible Assumption in Bernoulli's Equation

Bernoulli's equation assumes incompressible flow. For liquids like water, this is generally accurate. For gases, this assumption is only valid at low velocities (Mach number < 0.3) where density changes are negligible.

Impulse-Momentum Principle

Derived from Newton's Second Law (F=maF=ma). It states that the sum of external forces acting on a fluid control volume equals the rate of change of momentum.

Impulse-Momentum Equation

Calculates the forces exerted by or on a fluid control volume due to momentum changes.

โˆ‘Fโƒ—=ฯQ(Vโƒ—outโˆ’Vโƒ—in)\sum \vec{F} = \rho Q (\vec{V}_{out} - \vec{V}_{in})

Variables

SymbolDescriptionUnit
Sum of external forces acting on the fluidN
Fluid densitykg/m3kg/m^3
QQVolumetric flow ratem3/sm^3/s
Outlet velocity vectorm/s
Inlet velocity vectorm/s

Guidelines for Applying Impulse-Momentum

Analysis guidelines for the impulse-momentum principle:

  • โˆ‘Fโƒ—\sum \vec{F} includes pressure forces, weight, and reaction forces from boundaries (e.g., pipe bends).
  • Vector equation: Solve for X and Y components separately.

Forces Exerted by Jets

The impulse-momentum principle is applied to calculate the force of a fluid jet striking a surface.

Jet Deflection Overview

When a fluid jet of cross-sectional area AA and velocity VV strikes a stationary flat plate or curved vane, it exerts a force due to the change in momentum. We analyze the forces for two main cases:

  • Stationary Flat Plate Normal to Jet: Where all forward momentum is destroyed in the direction of the jet.
  • Stationary Curved Vane: Where the jet is deflected by an angle ฮธ\theta from its original direction.

Stationary Flat Plate Normal to Jet

Calculates the force exerted by a jet striking a flat stationary surface at a right angle.

F=ฯAV2=ฯQVF = \rho A V^2 = \rho Q V

Variables

SymbolDescriptionUnit
FFNormal force on the plateN
Fluid densitykg/m3kg/m^3
AACross-sectional area of the jetm2m^2
VVVelocity of the jetm/s
QQVolumetric flow ratem3/sm^3/s

Stationary Curved Vane - Horizontal Force

Calculates the horizontal component of the force exerted by a deflected jet on a stationary curved vane.

Fx=ฯQV(1โˆ’cosโกฮธ)F_x = \rho Q V (1 - \cos\theta)

Variables

SymbolDescriptionUnit
FxF_xForce component in the direction of the jetN
Fluid densitykg/m3kg/m^3
QQVolumetric flow ratem3/sm^3/s
VVVelocity of the jetm/s
Deflection angle of the vanedegrees

Stationary Curved Vane - Vertical Force

Calculates the vertical component of the force exerted by a deflected jet on a stationary curved vane.

Fy=โˆ’ฯQVsinโกฮธF_y = -\rho Q V \sin\theta

Variables

SymbolDescriptionUnit
FyF_yForce component perpendicular to the jet directionN
Fluid densitykg/m3kg/m^3
QQVolumetric flow ratem3/sm^3/s
VVVelocity of the jetm/s
Deflection angle of the vanedegrees

Moving Vanes (Pelton Wheel Principle)

If a curved vane moves in the same direction as the jet with velocity uu (where u<Vu < V), the force is dictated by the relative velocity of the fluid relative to the vane (Vr=Vโˆ’uV_r = V - u). The mass flow rate actually striking the vane is also reduced to mห™=ฯA(Vโˆ’u)\dot{m} = \rho A (V - u).

Force on a Moving Curved Vane

Calculates the force exerted in the direction of vane movement.

Fx=ฯA(Vโˆ’u)2(1โˆ’cosโกฮธ)F_x = \rho A (V - u)^2 (1 - \cos\theta)

Variables

SymbolDescriptionUnit
FxF_xForce component in the direction of motionN
Fluid densitykg/m3kg/m^3
AACross-sectional area of the jetm2m^2
VVAbsolute velocity of the jetm/s
uuVelocity of the moving vanem/s
Deflection angle of the vanedegrees

Jet Power on Moving Vanes

The mechanical power generated by the jet striking the moving vane is P=FxuP = F_x u. This is the fundamental operating principle of impulse turbines such as the Pelton wheel.

Key Takeaways
  • Euler's Equation is the differential form of motion for an inviscid fluid. Integrating it yields Bernoulli's equation.
  • Bernoulli's Equation applies to steady, incompressible, frictionless flow along a streamline, acting as a statement of conservation of mechanical energy.
  • It states that the sum of pressure head, velocity head, and elevation head is constant.
  • The Energy Line (EL) represents total head and is horizontal for ideal flow, while the Hydraulic Grade Line (HGL) represents piezometric head and is lower than the EL by the velocity head.
  • The Navier-Stokes Equations extend fluid dynamic analysis to real, viscous fluids by including internal friction (viscous forces).
  • They are based on Newton's Second Law and represent a complex balance of inertial, pressure, viscous, and body forces.
  • Torricelli's Theorem shows that fluid exiting an orifice has a velocity proportional to the square root of the depth (V=2ghV = \sqrt{2gh}), similar to a freely falling body.
  • Venturi Meters measure flow rate accurately by creating a constriction that increases velocity and decreases pressure, with minimal permanent head loss.
  • Pitot Tubes measure local point velocity by bringing the fluid to a dead stop and measuring the resulting stagnation pressure.
  • The Impulse-Momentum Equation is used to calculate forces exerted by moving fluids on solid boundaries, such as pipe bends, nozzles, or turbine blades.
  • It is a vector equation, meaning forces and velocities must be analyzed in their respective X, Y, and Z components.