INGENIA

FLD-18

Navier–Stokes inertial–viscous snapshot

Re = ρ U L / μ compares ρ(u·∇)u with μ ∇²u. The local inertial-to-viscous ratio.

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FluidsNavier–Stokes

Governing equation

Re=ρULμ∼∣ρ(u⋅∇)u∣∣μ∇2u∣Re=\dfrac{\rho U L}{\mu}\sim\dfrac{|\rho(\mathbf u\cdot\nabla)\mathbf u|}{|\mu\nabla^2\mathbf u|}

U∈[0.01,40]U \in \left[0.01, 40\right]

where

\rho
Density (kg/m³)
U
Scale speed (m/s)
L
Scale length (m)
\mu
Viscosity (Pa·s)
Re
Inertia / viscous (—)
F_{in}/V
Inertial density (N/m³)
F_{vis}/V
Viscous density (N/m³)

The figure, part by part

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FLD-18 · pipe
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①

Governing law — red

Re=ρULμ∼∣ρ(u⋅∇)u∣∣μ∇2u∣Re=\dfrac{\rho U L}{\mu}\sim\dfrac{|\rho(\mathbf u\cdot\nabla)\mathbf u|}{|\mu\nabla^2\mathbf u|}

U∈[0.01,40]U \in \left[0.01, 40\right]

U=0.01U = 0.01Re=1000Re = 1000

②

Domain of the variable — blue

Umin⁡=0.01,Umax⁡=40U_{\min} = 0.01,\quad U_{\max} = 40

U∈[0.01,40]U \in \left[0.01, 40\right]

U=0.01U = 0.01U=0.01U = 0.01

③

Response curve — green

Re=ρULμ∼∣ρ(u⋅∇)u∣∣μ∇2u∣Re=\dfrac{\rho U L}{\mu}\sim\dfrac{|\rho(\mathbf u\cdot\nabla)\mathbf u|}{|\mu\nabla^2\mathbf u|}

U∈[0.01,40]U \in \left[0.01, 40\right]

U=0.01U = 0.01Re=1000Re = 1000

④

Rate of change — amber

dRedU\frac{\mathrm{d}Re}{\mathrm{d}U}

U∈[0.01,40]U \in \left[0.01, 40\right]

U=0.262U = 0.262Re′=1×105Re^{\prime} = 1\times 10^{5}

Lecture brief

Historical brief

Bernoulli, Navier–Stokes, Reynolds (1883) and Stokes drag made continuum flow a dimensionless craft. The sheets compute head, drag, Re and a pedagogical NS snapshot. This sheet (FLD-18 — Navier–Stokes inertial–viscous snapshot) is the form associated with Navier–Stokes. Working symbols: ρ\rho, UU, LL, μ\mu →\rightarrow ReRe, Fin/VF_{in}/V, Fvis/VF_{vis}/V. The incompressible NS equation is ∂u/∂t + (u·∇)u = −∇p/ρ + ν∇²u. This sheet is one scale estimate.

Purpose

Purpose: compute ReRe, Fin/VF_{in}/V, Fvis/VF_{vis}/V from ρ\rho, UU, LL, μ\mu in Fluid physics via Re=ρULμ∼∣ρ(u⋅∇)u∣∣μ∇2u∣Re=\dfrac{\rho U L}{\mu}\sim\dfrac{|\rho(\mathbf u\cdot\nabla)\mathbf u|}{|\mu\nabla^2\mathbf u|} Re = ρ U L / μ compares ρ(u·∇)u with μ ∇²u. The local inertial-to-viscous ratio. Use it when a real fluid physics question must be answered in SI before a code check.

Live realistic example

In symbols

Live case. Given ρ=1000.000 kg/m3\rho = 1000.000\,\mathrm{kg/m^{3}}, U=1.000 m/sU = 1.000\,\mathrm{m/s}, L=0.100 mL = 0.100\,\mathrm{m}, μ=0.001 Pa⋅s\mu = 0.001\,\mathrm{Pa·s}, the governing relation Re=ρULμ∼∣ρ(u⋅∇)u∣∣μ∇2u∣Re=\dfrac{\rho U L}{\mu}\sim\dfrac{|\rho(\mathbf u\cdot\nabla)\mathbf u|}{|\mu\nabla^2\mathbf u|} yields Re=100000.00 —Re = 100000.00\,\mathrm{—}, Fin/V=10000.00 N/m3F_{in}/V = 10000.00\,\mathrm{N/m^{3}}, Fvis/V=0.10 N/m3F_{vis}/V = 0.10\,\mathrm{N/m^{3}}. A blob of fluid, two force arrows, a Re bar. Move a slider: the numbers are this situation, not a canned story.

Calculator

Inputs

Outputs

  • Inertia / viscous Re100000.00 —
  • Inertial density F_{in}/V10000.00 N/m³
  • Viscous density F_{vis}/V0.10 N/m³
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FLD-18 · pipe
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Narration of this film

A blob of fluid, two force arrows, a Re bar.

The incompressible NS equation is ∂u/∂t + (u·∇)u = −∇p/ρ + ν∇²u. This sheet is one scale estimate.

Reading speed

Watch on YouTube