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Turbulence k-Epsilon Boundary Calculator engineering
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Turbulence k-Epsilon Boundary Calculator

Computational fluid dynamics & boundary specification: Calculate turbulent kinetic energy ($k$), dissipation rate ($ arepsilon$), specific dissipation ($omega$), and eddy viscosity ratio ($mu_t / mu$).

Inlet Inflow & Geometric Scales

Inlet bulk flow velocity
Low < 1%, Medium 5%, High > 10%
Geometry definition
D_h or turbulent eddy scale ℓ
Air ~1.5e-5, Water ~1.0e-6 m²/s
Standard k-ε closure (0.09)

Inlet Boundary Variables

Turbulent Kinetic Energy (k)
-
k = ³/₂ · (U · I)² (m²/s²)
Dissipation Rate (ε)
-
ε = C_μ^(¾) · k^(1.5) / ℓ (m²/s³)
Specific Dissipation (ω)
-
ω = k^(½) / (C_μ^¼ · ℓ) (s⁻¹)
Eddy Viscosity Ratio (μ_t / μ)
-
Turbulent / Molecular viscosity
Turbulent Length Scale (ℓ)
-
Integral eddy size
Turbulent Velocity RMS (u')
-
Fluctuating velocity scale

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Frequently Asked Questions

What is typical turbulence intensity for external aerodynamics?

For external vehicle aerodynamics (automotive, aerospace flight), free-stream turbulence intensity is typically low (I ≈ 0.1% to 1.0%). For internal combustion engine manifolds, turbomachinery, and heat exchangers, intensity is high (I ≈ 5% to 15%).

How does k decay between the inlet and the test object?

In empty domains, k and ε decay according to d(k)/dt = -ε. If the inlet is set far upstream of an airfoil, turbulence can decay by over 80% before reaching the leading edge. Modified ambient source terms or shorter inlet distances prevent this decay.

Can k and ω be directly transferred into OpenFOAM?

Yes. In OpenFOAM, specify type "turbulentIntensityKineticEnergyInlet" for k and "turbulentMixingLengthDissipationRateInlet" for epsilon/omega, using the exact values computed above in the 0/ folder.