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 Boundary Variables
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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.