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Technical Terms Fluid Mechanics

Reference data and engineering information about technical terms fluid mechanics for fluid mechanics applications.

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Overview

Engineering reference data for Technical Terms Fluid Mechanics in fluid mechanics.

Key Formulas

Reynolds Number

Re=ρvDμRe = \frac{\rho v D}{\mu}

Ratio of inertial to viscous forces — determines flow regime.

Bernoulli's Equation

P+12ρv2+ρgh=constP + \frac{1}{2}\rho v^2 + \rho g h = \text{const}

Conservation of energy for steady, inviscid, incompressible flow.

Continuity Equation

A1v1=A2v2A_1 v_1 = A_2 v_2

Conservation of mass for incompressible flow.

Darcy-Weisbach

ΔP=fLDρv22\Delta P = f \frac{L}{D} \frac{\rho v^2}{2}

Pressure drop due to friction in a pipe.

Variables

Symbol Description Unit
ReRe Reynolds number
ρ\rho Fluid density kg/m³
vv Flow velocity m/s
DD Characteristic dimension m
μ\mu Dynamic viscosity Pa·s
PP Pressure Pa
ff Darcy friction factor

Glossary of Key Terms

Acoustic Theory

The mathematical description of sound waves, fundamental to acoustical engineering and noise control in HVAC systems.

Aerodynamics

The study of the flow of gases, particularly as it relates to the design of vehicles and structures moving through air.

Boundary Layer

The thin layer of fluid in the immediate vicinity of a bounding surface where viscous effects are significant. The boundary layer can be laminar, transitional, or turbulent.

Cavitation

The formation and collapse of vapor bubbles in a liquid when local pressure drops below the vapor pressure. Characterized by Net Positive Suction Head (NPSH) requirements in pump systems.

Coanda Effect

The tendency of a fluid stream to stay attached to a convex surface rather than follow its original straight-line trajectory.

Conservation Laws

Fundamental principles stating that measurable properties of an isolated physical system (mass, energy, momentum) remain constant as the system evolves.

Froude Number

A dimensionless number defined as the ratio of flow inertia to gravitational forces:

Fr=vgLFr = \frac{v}{\sqrt{gL}}

where vv is flow velocity, gg is gravitational acceleration, and LL is characteristic length.

Euler Number

A dimensionless number representing the relationship between pressure forces and inertial forces:

Eu=Δpρv2Eu = \frac{\Delta p}{\rho v^2}

Hydraulics

The branch of science and engineering concerned with the mechanical properties and use of liquids, particularly water.

Hydrodynamics

Fluid dynamics applied specifically to liquids such as water, alcohol, and oil.


Dimensionless Numbers Reference

Number Formula Ratio Application
Froude Fr=v/gLFr = v/\sqrt{gL} Inertia to gravity Free-surface flows
Euler Eu=Δp/(ρv2)Eu = \Delta p/(\rho v^2) Pressure to inertia Pressure drop analysis
Reynolds Re=ρvL/μRe = \rho vL/\mu Inertia to viscosity Flow regime determination

Flow Regime Classification

Fluid flow can be classified based on the Reynolds number:

Flow Type Reynolds Number Range Characteristics
Laminar Re<2300Re < 2300 Smooth, orderly layers
Transitional 2300<Re<40002300 < Re < 4000 Intermittent turbulence
Turbulent Re>4000Re > 4000 Chaotic, mixing occurs

Conservation of Mass

The law of conservation of mass states that mass can neither be created nor destroyed. For fluid mechanics, this is expressed through the continuity equation:

ρt+(ρv)=0\frac{\partial \rho}{\partial t} + \nabla \cdot (\rho \mathbf{v}) = 0

For incompressible flow (ρ=constant\rho = \text{constant}), this simplifies to:

v=0\nabla \cdot \mathbf{v} = 0


Viscosity Types

Type Symbol SI Unit Description
Dynamic (Absolute) μ\mu Pa·s Resistance to shear stress
Kinematic ν\nu m²/s Dynamic viscosity divided by density

The relationship between viscosity types:

ν=μρ\nu = \frac{\mu}{\rho}

Common unit conversions:

  • 1 cP (centipoise) = 0.001 Pa·s
  • 1 cSt (centistoke) = 10⁻⁶ m²/s

Flow Coefficient Standards

Standard Symbol Definition Region
US CvC_v Flow rate (gpm) at 1 psi differential North America
International KvK_v Flow rate (m³/h) at 1 bar differential Europe/Asia

Conversion between standards:

Kv=0.857×CvK_v = 0.857 \times C_v

References