Reynolds Number
\[Re=\frac{\rho VD}{\mu}\]

Variables

ReReynolds number
rho[ρ]fluid density (kg/m³)
Vfluid velocity (m/s)
Dcharacteristic length (m)
mu[μ]dynamic viscosity (Pa·s)

Description

What is this formula?


The Reynolds Number is a dimensionless quantity that compares inertial forces to viscous forces within a fluid flow.


It is one of the most important parameters in fluid mechanics because it helps determine whether a flow is laminar, transitional, or turbulent.


When to use it


Use this formula when analyzing fluid flow around aircraft, wings, pipes, turbines, vehicles, or any engineering system involving moving fluids.


It is widely used in aerodynamics, hydrodynamics, heat transfer, and CFD simulations.


Example


Air flows over an airfoil with:


Density = 1.225 kg/m³


Velocity = 50 m/s


Characteristic length = 1.5 m


Dynamic viscosity = 1.81×10^-5 Pa·s


Formula:


Re = (ρ × V × D) / μ


Substitution:


Re = (1.225 × 50 × 1.5) / (1.81×10^-5)


Re = 5.08×10^6


Result:


Reynolds number = 5.08 million


Applications


Aircraft wing analysis


Wind tunnel testing


CFD model scaling


Pipe flow calculations


Heat transfer analysis


Aerospace engineering


Note


The Reynolds number is not a physical property but a dimensionless similarity parameter. Critical Reynolds values depend on geometry, surface roughness, and flow conditions. Different engineering applications may use different characteristic lengths when calculating Reynolds number.

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