100,000
0.000001
m²/s
—
100,000
0.000001
m²/s
—
The Reynolds Number Calculator computes the dimensionless Reynolds number (Re) that predicts whether a fluid flow will be laminar, transitional, or turbulent. Named after Osborne Reynolds, this parameter is perhaps the single most important dimensionless number in fluid mechanics, governing everything from pipe design to aerodynamic analysis.
Enter the fluid properties and flow conditions to determine Re and the expected flow regime.
The Reynolds number is defined as the ratio of inertial forces to viscous forces:
$$Re = \frac{\rho v D}{\mu} = \frac{v D}{\nu}$$
where:
The flow regime classification for internal pipe flow:
The physical interpretation is straightforward: when inertial forces dominate (high Re), the flow cannot remain orderly and becomes turbulent. When viscous forces dominate (low Re), they damp disturbances and maintain laminar flow.
Different geometries have different critical Reynolds numbers. For flow over a flat plate, transition occurs around Re ≈ 500,000. For flow around a sphere, the drag crisis occurs near Re ≈ 200,000. The values 2,300 and 4,000 apply specifically to pipe flow.
A high Reynolds number means the flow is dominated by inertia and likely turbulent — expect higher friction losses but better mixing. A low Reynolds number indicates viscous-dominated laminar flow — lower friction but poor mixing. For engineering design, knowing the flow regime is essential for selecting the correct friction factor, heat transfer correlations, and mixing models.
Inputs
Results
Water at 20°C flowing at 1.5 m/s through a 25 mm pipe has Re ≈ 37,400 — clearly turbulent, typical for plumbing.
Inputs
Results
Honey (μ ≈ 5 Pa·s) at 1 cm/s in a 50 mm tube has Re ≈ 0.14 — extremely laminar due to high viscosity.
The units cancel out: (kg/m³)(m/s)(m)/(Pa·s) = (kg/m³)(m/s)(m)/(kg/(m·s)) = 1. Dimensionless numbers allow comparison across different scales and fluids — a key principle of dimensional analysis and similitude.
For circular pipes, use the internal diameter. For non-circular ducts, use the hydraulic diameter Dh = 4A/P (where A is cross-sectional area and P is wetted perimeter). For external flows, use the body length or diameter.
In practice, disturbances from rough walls, vibrations, or inlet conditions can trigger turbulence below Re = 2,300, though it is difficult to maintain. Conversely, in very smooth pipes with careful inlet conditions, laminar flow has been observed up to Re ≈ 100,000.
Air at 20°C has ρ ≈ 1.2 kg/m³ and μ ≈ 1.81 × 10⁻⁵ Pa·s. For air at 10 m/s through a 0.1 m duct: Re = 1.2 × 10 × 0.1 / 1.81e-5 ≈ 66,300 (turbulent).
Temperature changes viscosity significantly. For liquids, viscosity decreases with temperature (increasing Re). For gases, viscosity increases with temperature (decreasing Re). Always use viscosity values at the actual fluid temperature.
Kinematic viscosity ν = μ/ρ combines dynamic viscosity and density into a single property. It represents the ratio of viscous diffusion to fluid volume. Water at 20°C has ν ≈ 1.0 × 10⁻⁶ m²/s, while air has ν ≈ 1.5 × 10⁻⁵ m²/s.
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