Re = ρ·v·D / μRe = v·D / ν  ·  ν = μ / ρ  ·  laminar Re < 2,300  ·  turbulent Re > 4,000

The Reynolds number compares the inertia of a moving fluid with its viscosity, Re = ρ·v·D / μ, and every unit cancels out. This free Reynolds number calculator returns Re from the density, mean velocity, pipe inside diameter and dynamic viscosity, or solves for the velocity, diameter or viscosity that gives a chosen Re, and tells you whether the flow is laminar or turbulent.

Load a real case

Each button writes a density, a mean velocity, a diameter and a viscosity into the boxes above and lets the calculator do the rest. The confirmation line quotes the result the engine renders, not a stored answer.

Pick a case above, or type your own numbers.

What Is the Reynolds Number Calculator?

The Reynolds number calculator is a free online tool built on the definition Re = ρ·v·D / μ. Enter the fluid's density and dynamic viscosity, the mean velocity and the pipe inside diameter, in whichever units suit you, and it returns the Reynolds number with every step of the substitution, or solves for the velocity, diameter or viscosity that gives a chosen Re. The flow regime, the kinematic viscosity and the smooth-pipe friction factor appear alongside the result.

Variables used by the Reynolds number calculator
SymbolQuantityDefault unitAlso acceptsExample value
ρDensitykg/m³g/cm³998.2
vMean velocitym/scm/s, km/h, ft/s1
DPipe inside diametermmcm, m, in25
μDynamic viscositymPa·sPa·s, cP, Poise1.002

How to use the Reynolds number calculator

  1. Pick the unknown. The Solve for menu offers Reynolds number (Re), the default, or Mean velocity (v), Pipe inside diameter (D) and Dynamic viscosity (μ) for the inverse problems. Whichever you choose, Density stays on the form as an input.
  2. Enter the fluid. Type the density in kg/m³ or g/cm³ and the dynamic viscosity in mPa·s, Pa·s, cP or Poise; 1 cP is exactly 1 mPa·s, so a centipoise table goes straight in. The defaults are water at 20 °C, 998.2 kg/m³ and 1.002 mPa·s.
  3. Enter the velocity and the diameter. The Mean velocity is the volumetric flow rate divided by the pipe's cross-sectional area, in m/s, cm/s, km/h or ft/s. The Pipe inside diameter is the bore, not the nominal size or the outside diameter, in mm, cm, m or inches.
  4. Read the result and the extras. The answer shows with the working underneath, followed by the flow regime, the kinematic viscosity ν = μ/ρ, the Darcy friction factor for a smooth pipe with the formula it came from, and the thresholds used to name the regime.

The common mistake is the viscosity unit: water is 1.002 mPa·s, and typing 1.002 with Pa·s selected makes it a thousand times too thick, so a turbulent supply pipe comes out laminar with Re near 25. The second is the velocity: enter the mean value, the flow rate over the area, not the centreline speed, which is twice the mean in laminar flow.

Reynolds number calculator at its default inputs: density 998.2 kg/m³, mean velocity 1 m/s, pipe inside diameter 25 mm and dynamic viscosity 1.002 mPa·s give a Reynolds number of 24905, with extras reading Turbulent (Re > 4,000), kinematic viscosity 1.004e-6 m²/s and a smooth-pipe Darcy friction factor of 0.02515 (Blasius).
The default case. Water at 20 °C moving at 1 m/s through a 25 mm pipe returns a Reynolds number of 24905, and the extras beneath the result say what that means: the flow is turbulent, the kinematic viscosity is 1.004e-6 m²/s and the smooth-pipe friction factor from the Blasius fit is 0.02515.

Worked example: change one thing at a time

Start from the page defaults and move as little as possible per row. Every figure in the table is the string the calculator itself displays for those inputs, so if the table and the tool ever disagree, the tool is right.

What the calculator reports as each input moves
Step Density Mean velocity Inside diameter Dynamic viscosity Reynolds number Flow regime Kinematic viscosity Friction factor, smooth pipe
Start (page defaults) 998.2 kg/m³ 1 m/s 25 mm 1.002 mPa·s 24905 Turbulent (Re > 4,000) 1.004e-6 m²/s 0.02515 (Blasius)
Slow the water to 0.05 m/s 998.2 kg/m³ 0.05 m/s 25 mm 1.002 mPa·s 1245.3 Laminar (Re < 2,300) 1.004e-6 m²/s 0.05139 (64/Re)
Water at 0.1 m/s 998.2 kg/m³ 0.1 m/s 25 mm 1.002 mPa·s 2490.5 Transitional (2,300 to 4,000) 1.004e-6 m²/s n/a in transition
Air duct preset 1.204 kg/m³ 5 m/s 100 mm 0.01825 mPa·s 32986 Turbulent (Re > 4,000) 1.516e-5 m²/s 0.02345 (Blasius)
Glycerine preset 1261 kg/m³ 0.1 m/s 10 mm 1412 mPa·s 0.89306 Laminar (Re < 2,300) 1.120e-3 m²/s 71.66 (64/Re)
SAE 30 oil preset 876 kg/m³ 0.5 m/s 50 mm 83.2 mPa·s 263.22 Laminar (Re < 2,300) 9.498e-5 m²/s 0.2431 (64/Re)
Water main, 2 m/s in 500 mm 998.2 kg/m³ 2 m/s 500 mm 1.002 mPa·s 996210 Turbulent (Re > 4,000) 1.004e-6 m²/s 0.01159 (Haaland)

Rows 1 to 3 keep water in the same 25 mm pipe and change only the speed: at 1 m/s the flow is turbulent with Re near 25,000, at 0.05 m/s it is laminar at 1,245, and 0.1 m/s lands in the transition band at 2,490, where the calculator declines to quote a friction factor. Re scales in direct proportion to v, D and ρ and in inverse proportion to μ, which is why the glycerine row, some 1,400 times more viscous than water, stays below 1 even though the fluid is a quarter denser.

Rows 4 to 6 are the presets. Air is about 55 times less viscous than water but 830 times less dense, so a modest 5 m/s in a 100 mm duct still reaches 32,986 and is firmly turbulent, while the oil line sits laminar at 263. Row 7 pushes a 500 mm main to 2 m/s and passes 100,000, where the friction factor switches from the Blasius fit to the Haaland smooth-pipe equation.

Run the inverse to close the loop. Choose Mean velocity (v), enter 24905.2 for the Reynolds number with the water defaults, and the calculator returns 1 m/s; Pipe inside diameter (D) returns 25 mm and Dynamic viscosity (μ) returns 1.002 mPa·s, the row 1 inputs recovered exactly. Solving for velocity with Re = 2300 gives 0.09235 m/s, the speed below which 20 °C water in a 25 mm pipe is laminar, and Re = 4000 gives 0.16061 m/s, above which it is turbulent.

Formula and symbol reference

Everything the tool computes comes from one definition, Re = ρ·v·D / μ, and its three rearrangements v = Re·μ / (ρ·D), D = Re·μ / (ρ·v) and μ = ρ·v·D / Re. The extras add ν = μ / ρ and the smooth-pipe friction factor for whichever regime the result falls in.

Symbols, units and working ranges
Symbol Meaning SI unit Typical range
Re Reynolds number, the ratio of inertial to viscous forces; the result when solving for Re and an input otherwise none (dimensionless) Below 1 for the slow flow of a viscous fluid, 2,300 to 4,000 through the transition band, tens of thousands to over a million in water and air pipework.
ρ Fluid density kilogram per cubic metre, kg/m³ 1.204 kg/m³ for air and 998.2 kg/m³ for water at 20 °C; most liquids sit between 700 and 1,300 kg/m³, glycerine at 1,261.
v Mean velocity: the volumetric flow rate divided by the cross-sectional area metre per second, m/s Commonly 0.5 to 3 m/s in water pipework and 3 to 20 m/s in ventilation ducts. Enter the mean, not the centreline value.
D Pipe inside diameter, the bore; for a non-circular duct use the hydraulic diameter 4A/P metre, m 10 mm to 500 mm in the examples on this page. Enter mm, cm or inches and the tool converts.
μ Dynamic (absolute) viscosity at the working temperature pascal second, Pa·s 0.01825 mPa·s for air and 1.002 mPa·s for water at 20 °C; 83.2 mPa·s for SAE 30 oil at 40 °C; 1,412 mPa·s for glycerine at 20 °C.
ν Kinematic viscosity μ/ρ, reported as an extra square metre per second, m²/s 1.004e-6 m²/s for water and 1.516e-5 m²/s for air at 20 °C. 1 cSt = 1e-6 m²/s.
f Darcy friction factor for a hydraulically smooth pipe, reported as an extra none (dimensionless) 64/Re below 2,300 (0.05139 at Re = 1,245); Blasius 0.316·Re^(-1/4) from 4,000 to 100,000 (0.02515 at Re = 24,905); Haaland above 100,000; not quoted in the transition band.

The physics: what the extras are telling you

The ratio ρ·v·D/μ weighs the inertia of the moving fluid against the viscous stresses that resist it; the guide linked under Where to go next derives it and tells the story of the 1883 dye experiment. What matters here is how the calculator turns that single number into the extras beneath the result.

Below 2,300 it labels the flow Laminar and quotes f = 64/Re, the exact Poiseuille result for orderly layered flow in which the centreline runs at twice the mean velocity. Above 4,000 it labels the flow Turbulent, where eddies mix momentum across the pipe and flatten the profile to about 1.2 times the mean, and quotes the Blasius fit f = 0.316·Re^(-1/4) up to Re = 100,000 and the Haaland smooth-pipe equation beyond it.

The thresholds are conventions with a margin built in. Turbulent puffs can persist down to roughly Re 2,000 in a disturbed flow, 2,300 is the conventional design limit, and between 2,300 and 4,000 the calculator reports Transitional and prints n/a for the friction factor, because neither the laminar nor the turbulent formula is reliable there.

The kinematic viscosity extra, ν = μ/ρ, is the same information in another form: Re = v·D/ν, which is the version to reach for when a data sheet quotes centistokes (1 cSt = 1e-6 m²/s). Density and viscosity enter only through that ratio, so a fluid that is both dense and viscous, like glycerine, still sits far below water on the Reynolds scale.

Reynolds number calculator loaded with the air duct preset: density 1.204 kg/m³, mean velocity 5 m/s, pipe inside diameter 100 mm and dynamic viscosity 0.01825 mPa·s return a Reynolds number of 32986, with extras reading Turbulent (Re > 4,000), kinematic viscosity 1.516e-5 m²/s and a smooth-pipe Darcy friction factor of 0.02345 (Blasius).
The Air duct preset. Air is far less viscous than water but also far less dense, and the two nearly cancel: 5 m/s through a 100 mm duct gives 32986, turbulent, with a kinematic viscosity of 1.516e-5 m²/s, about fifteen times that of water.

Where the formula breaks down

The Reynolds number is exact as a definition; it is the regime labels and the friction factor that carry assumptions. Each of the cases below changes what the number means, and each has a recognisable symptom.

Non-circular ducts
D is the inside diameter of a circular pipe. For a rectangular duct or an annulus use the hydraulic diameter 4A/P, four times the flow area divided by the wetted perimeter; the thresholds then hold only approximately, so verify against duct-flow data before relying on a result near them.
The transition band is not a switch
2,300 and 4,000 are conventions with a margin built in, not laws of nature. Turbulent puffs can persist down to roughly Re 2,000 in a disturbed flow, so 2,300 is the conventional design limit rather than a hard floor, while with a very smooth inlet and a quiet supply laminar flow has been kept well beyond 10,000 in the laboratory; treat any result close to the thresholds as uncertain.
Symptom: a measured pressure drop that sits between the laminar and turbulent predictions, or one that changes from run to run at the same flow.
Temperature changes the viscosity
Viscosity is the most temperature-sensitive input. Water falls from 1.002 mPa·s at 20 °C to about 0.89 mPa·s at 25 °C, roughly 2 per cent per degree, and lubricating oils change far faster, so use the viscosity at the working temperature rather than a room-temperature table value.
Non-Newtonian fluids
The formula assumes a Newtonian fluid, one whose viscosity does not depend on how fast it is sheared. Paints, slurries, polymer solutions and blood in small vessels all break that assumption, and a Reynolds number for them needs an apparent viscosity at the relevant shear rate, which this calculator cannot supply.
Rough walls
The friction factor extra assumes a hydraulically smooth wall. Commercial steel, cast iron and concrete are rough enough to raise f noticeably in turbulent flow; take the Reynolds number from here to the friction factor calculator, which accepts the relative roughness ε/D and solves the Colebrook equation.
Developing flow near an inlet
Re describes fully developed flow. Just downstream of an inlet, bend or valve the velocity profile is still forming over an entrance length of about 0.06·Re·D in laminar flow, which for the 0.05 m/s water example is roughly 1.9 m of pipe, so a short run may never reach the profile the regime label implies.
Gases at high speed
For a gas moving fast, the density is no longer constant along the pipe. Below about a third of the speed of sound the error is small, but beyond that the Reynolds number alone no longer characterises the flow and the Mach number has to be considered as well.

Where it is actually used

Pipe sizing and pump head
Every pressure-drop calculation for a pipeline starts here. The Darcy-Weisbach equation needs f, f needs Re, so the engineer computes Re from the design flow, reads off the regime and only then picks a friction correlation; for the 25 mm domestic supply pipe at 1 m/s the tool gives turbulent flow with f = 0.02515, which works out at roughly 500 Pa of loss per metre of pipe.
Ventilation ducts
Air moves at a few metres per second through ducts hundreds of millimetres across, so almost every duct is turbulent; the air preset returns 32,986 for a 100 mm duct at 5 m/s. Designers rely on that to use turbulent friction charts throughout, and only check the laminar case for narrow instrument tubing.
Lubrication and oil lines
Oils are viscous enough that lines carrying them at moderate speed stay laminar, as the SAE 30 preset shows at Re = 263. In laminar flow the pressure drop is proportional to the velocity rather than its square, so doubling the flow doubles the loss, which is the arithmetic behind sizing hydraulic and lubrication lines. If the data sheet quotes centistokes, convert to mPa·s with the viscosity converter first.
Blood flow
Blood at a few millipascal seconds moving through the aorta, a vessel of roughly 25 mm, at a few tenths of a metre per second gives a Reynolds number in the low thousands, hovering around the laminar limit, while in the capillaries it is far below 1. The figures vary strongly between people and through the heartbeat, so verify any physiological value before use.
Microfluidics
In channels a few tens of micrometres across the Reynolds number is well below 1, so the flow is laminar whatever you do: two streams run side by side and mix only by diffusion. Lab-on-a-chip devices depend on that, and the calculator confirms it if you enter a 50 micrometre channel as 0.05 mm at a few millimetres per second.
Similarity and model testing
Two flows with the same Reynolds number and the same geometry behave the same way, which is how a scale model in a wind tunnel or a water channel stands in for the full-size object. Matching Re is the reason model tests run faster, use a denser fluid or pressurise the tunnel; solve for velocity here to see what speed a smaller diameter demands.
Reynolds number calculator loaded with the SAE 30 oil preset: density 876 kg/m³, mean velocity 0.5 m/s, pipe inside diameter 50 mm and dynamic viscosity 83.2 mPa·s return a Reynolds number of 263.22, with extras reading Laminar (Re < 2,300), kinematic viscosity 9.498e-5 m²/s and a smooth-pipe Darcy friction factor of 0.2431 (64/Re).
The SAE 30 oil preset. At 40 °C the oil is 83 times more viscous than water, so 0.5 m/s through a 50 mm line returns only 263.22: laminar, with the friction factor 0.2431 coming from the exact 64/Re result rather than a turbulent fit.

Where to go next

For the concept itself, Reynolds' dye experiment and worked problems, read the guide Reynolds Number: Formula and Meaning, and for the pressure and speed relation that friction loss competes with, the article on Bernoulli's principle. To carry the result forward, feed Re into the friction factor calculator for a rough pipe, or get μ from centistokes with the viscosity converter. Watch how viscosity shapes a flow in the viscosity simulator, or browse the library of physics simulations.

Frequently asked questions

What do the thresholds 2,300 and 4,000 mean?

Below a Reynolds number of about 2,300 flow in a circular pipe is laminar, above about 4,000 it is turbulent, and between the two it is transitional. The calculator labels the regime with those textbook thresholds, and in the transition band it withholds the friction factor because neither the laminar nor the turbulent formula is reliable. Turbulent puffs can persist down to roughly 2,000 in disturbed flow, so 2,300 is the conventional design limit with a margin built in.

What is the difference between laminar and turbulent flow?

Laminar flow moves in smooth parallel layers with a parabolic velocity profile, so the centreline runs at twice the mean speed and the pressure drop grows in proportion to the velocity. Turbulent flow is full of eddies that mix momentum across the pipe, flattening the profile to about 1.2 times the mean at the centre and making the pressure drop grow roughly with the square of the velocity.

Which diameter do I enter for a duct that is not circular?

Use the hydraulic diameter, four times the cross-sectional area divided by the wetted perimeter, in place of D. For a circular pipe this reduces to the inside diameter, for a square duct of side a it equals a, and for a wide flat channel it approaches twice the gap. The laminar and turbulent thresholds then apply only approximately, so verify against duct-flow data before relying on them.

Why is the Reynolds number dimensionless?

Because the units cancel: density in kg/m³ times velocity in m/s times diameter in m gives kg/(m·s), and dividing by a dynamic viscosity in Pa·s, which is also kg/(m·s), leaves a pure number. That is what makes it useful, since two flows with the same Re and the same shape behave alike whatever their size, speed or fluid. The calculator converts every input to SI before dividing, so the units you pick do not matter.

What is the difference between mPa·s, cP and Pa·s?

They are all units of dynamic viscosity, and 1 mPa·s is exactly 1 cP, so a centipoise table goes straight into the mPa·s box. 1 Pa·s is 1,000 mPa·s and 1 Poise is 0.1 Pa·s. Water at 20 °C is 1.002 mPa·s; entering 1.002 with Pa·s selected makes it a thousand times too viscous and turns a turbulent result laminar. Kinematic viscosity in centistokes must be multiplied by the density first.

Should I enter the mean velocity or the centreline velocity?

Enter the mean velocity: the volumetric flow rate divided by the pipe's cross-sectional area. In laminar flow the centreline moves at twice the mean, so a centreline reading would double the Reynolds number, and in turbulent flow it would overstate it by about 20 per cent. If you know the flow rate Q, the mean velocity is 4Q divided by π·D², with D the inside diameter.

References & formula source

  • Munson, Young & Okiishi — Fundamentals of Fluid Mechanics, Chapter 8 (Viscous flow in pipes: Reynolds number, laminar and turbulent regimes, friction factor).
  • White — Fluid Mechanics, Chapter 6 (Viscous flow in ducts; the Moody chart and the smooth-pipe correlations).
  • Halliday, Resnick & Walker — Fundamentals of Physics, Chapter 14 (Fluids).
  • Reynolds, O. (1883) — An experimental investigation of the circumstances which determine whether the motion of water shall be direct or sinuous, and of the law of resistance in parallel channels. Philosophical Transactions of the Royal Society of London, 174.
  • Further reading: Reynolds number — Wikipedia

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