Reynolds Number Calculator
Reynolds Number is evaluated from Fluid Velocity, Hydraulic Diameter and Fluid. The calculation reports Reynolds Number, Flow Regime and Darcy Friction Factor.
Results
About the Reynolds Number Calculator
The calculator uses a multi formula configuration. Each reported value is read as a direct evaluation of the stored rules with the declared field formats and units.
Formula basis:
Re = ρvD / mu (slug/ft^3, ft/s, ft, lb·s/ft^2)
Re = vD / ν (kinematic viscosity, ft^2/s)
Re < 2,300: Laminar → f = 64/Re
Re 2,300 - 4,000: Transitional
Re > 4,000: Turbulent → f approximately 0.316/Re^0.25
Interpret the outputs in the order shown by the result fields. Optional inputs affect only the outputs that depend on those variables.
Formula & How It Works
The calculation applies the following relations exactly as recorded in the metadata: Re = ρvD / mu (slug/ft^3, ft/s, ft, lb·s/ft^2) Re = vD / ν (kinematic viscosity, ft^2/s) Re < 2,300: Laminar → f = 64/Re Re 2,300 - 4,000: Transitional Re > 4,000: Turbulent → f approximately 0.316/Re^0.25 Each output field is produced by substituting the supplied inputs into the relevant relation and then applying the declared rounding or text format.
Worked Examples
Example 1: Residential Water Pipe — Laminar or Turbulent?
Inputs
With Fluid Velocity = 5, Hydraulic Diameter = 0.75 and Fluid = Water (60 degF): ρ=1.938, mu=2.35e-5 as the stated inputs, the result is Reynolds Number = 25,771, Flow Regime = Turbulent and Darcy Friction Factor = 0.02494. Each value corresponds to the declared output fields.
Example 2: HVAC Ductwork Air Flow
Inputs
With Fluid Velocity = 12, Hydraulic Diameter = 12 and Fluid = Air (68 degF): ρ=0.002378, mu=3.73e-7 as the stated inputs, the result is Reynolds Number = 989,617, Flow Regime = Turbulent and Darcy Friction Factor = 0.01002. Each value corresponds to the declared output fields.
Example 3: Laminar Flow — Slow Viscous Oil in Pipe
Inputs
With Fluid Velocity = 0.5, Hydraulic Diameter = 2, Fluid = Custom and Custom Density = 1.72 as the stated inputs, the result is Reynolds Number = 143, Flow Regime = Turbulent and Darcy Friction Factor = 0.03471. Each value corresponds to the declared output fields.
Example 4: Boeing 737 Wing — Boundary Layer Transition
Inputs
With Fluid Velocity = 440 and Fluid = Air (68 degF): ρ=0.002378, mu=3.73e-7 as the stated inputs, the result is Velocity = 134.112 m/s. Each value corresponds to the declared output fields.
Common Use Cases
- Determine if flow in a pipe is laminar or turbulent
- Calculate Reynolds number for water flowing through a duct
- Check transition from laminar to turbulent for air over a wing