Generalized Reynolds Number (Non‑Newtonian) Calculator

Analyze flow behavior across Newtonian and complex rheology models. Enter pipe size, velocity, and density with convenient unit conversions. Switch between power‑law, Herschel–Bulkley, Carreau, and Cross formulations. See generalized Reynolds, apparent viscosity, shear rate, and regime classification. Export results to CSV and downloadable PDF reports. Built for fast, dependable engineering workflow decisions daily.

Inputs (SI is used internally; choose your preferred units)
Fluid mass density.
Cross‑sectional average.
Hydraulic diameter.

Choose constitutive relation.
e.g., water ≈ 0.001 Pa·s at 20 °C.
Results
Generalized Re
(—)
Apparent viscosity, μapp
Pa·s
Wall shear rate, γw
s⁻¹
Regime
Example data
# Model ρ [kg/m³] v [m/s] D [m] Params μapp [Pa·s] Re (generalized)
Click a row to load its values into the form.
Formulas used

Wall shear rate: For laminar, circular pipe, Newtonian baseline uses \( \gamma_w \approx \dfrac{8v}{D} \). For power‑law and many shear‑dependent fluids, the Metzner–Reed correction gives \( \gamma_w \approx \dfrac{8v}{D}\,\dfrac{3n+1}{4n} \).

Generalized Reynolds number (apparent‑viscosity basis): \( \displaystyle \mathrm{Re}_g = \frac{\rho\,v\,D}{\mu_{\mathrm{app}}} \), where \( \mu_{\mathrm{app}} \) is the viscosity evaluated at the chosen shear rate.

  • Newtonian: \( \mu_{\mathrm{app}} = \mu \), so \( \mathrm{Re}=\rho v D/\mu \).
  • Power‑law: \( \mu_{\mathrm{app}} = K\,\gamma_w^{\,n-1} \).
  • Herschel–Bulkley: \( \mu_{\mathrm{app}} = \tau_y/\gamma_w + K\,\gamma_w^{\,n-1} \).
  • Carreau–Yasuda: \( \mu = \mu_\infty + (\mu_0-\mu_\infty)\,\big[1+(\lambda\gamma)^{a}\big]^{\frac{n-1}{a}} \).
  • Cross: \( \mu = \mu_\infty + \dfrac{\mu_0-\mu_\infty}{1+(\lambda\gamma)^{m}} \).

Metzner–Reed generalized Reynolds (power‑law): \( \displaystyle \mathrm{Re}_{g,\mathrm{MR}}= \frac{\rho\,v^{\,2-n} D^{\,n}}{K\,8^{\,n-1}\left(\frac{3n+1}{4n}\right)^{\,n-1}} \). This reduces to the classical definition at \(n=1\).

Regime hint: As a practical guide, laminar if \(\mathrm{Re}_g\lesssim 2100\), transitional for 2100–4000, turbulent if \(\mathrm{Re}_g\gtrsim 4000\). Thresholds vary slightly with rheology and entrance effects.

How to use
  1. Enter density, mean velocity, and pipe diameter using convenient units.
  2. Select a rheology model and provide the corresponding parameters.
  3. Press Calculate to compute wall shear rate, apparent viscosity, and Reynolds.
  4. Review the regime classification and, for power‑law, the Metzner–Reed value.
  5. Use the example rows to explore typical fluids; click to auto‑fill inputs.
  6. Export the example table as CSV or create a quick PDF summary.

All computations are performed in SI internally. Results are intended for steady, fully developed, incompressible, single‑phase pipe flow.

FAQs

It extends the classical Reynolds definition to non‑Newtonian fluids by using an appropriate apparent viscosity or, for power‑law, the Metzner–Reed expression that embeds shear‑rate corrections.

A common laminar estimate is \(8v/D\). For power‑law and related fluids, Metzner–Reed suggests multiplying by \((3n+1)/(4n)\). The tool applies these automatically for the supported models.

As a rule of thumb using the generalized Reynolds value: laminar < 2100, transitional 2100–4000, turbulent > 4000. Real thresholds depend on rheology, roughness, and entry length.

For power‑law fluids in pipes, Metzner–Reed is standard and aligns many friction‑factor correlations. The apparent‑viscosity form is more general for arbitrary viscosity models.

Yes. Set a flow index n > 1 for power‑law, or choose a Carreau/Cross parameter set that increases viscosity with shear rate.

Yes. Use Herschel–Bulkley and provide a nonzero yield stress. The tool treats yield via an apparent‑viscosity term \( \tau_y/\gamma_w \).

Assumes steady, fully‑developed, isothermal, single‑phase, incompressible pipe flow. Entrance effects, viscoelasticity, wall slip, and strong temperature variations are outside scope.

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Important Note: All the Calculators listed in this site are for educational purpose only and we do not guarentee the accuracy of results. Please do consult with other sources as well.