Numerical study of oscillating boundary layer flow over a flat plate using k–k–ω turbulence model

0202 electrical engineering, electronic engineering, information engineering 02 engineering and technology
DOI: 10.1016/j.ijheatfluidflow.2013.03.002 Publication Date: 2013-04-28T14:15:22Z
ABSTRACT
Abstract Oscillating boundary layer flow over an infinite flat plate at rest was simulated using the k – k L – ω turbulence model for a Reynolds number range of 32 ⩽  Re δ  ⩽ 10,000 ranging from fully laminar flow to fully turbulent flow. The k – k L – ω model was validated by comparing the predictions with LES results and experimental results for intermittently turbulent and fully turbulent flow regimes. The good agreement obtained between the k – k L – ω model prediction with the experimental and LES results indicate that the k – k L – ω model is able to accurately simulate transient intermittently turbulent flow and as well as accurately predict the onset of turbulence for such oscillatory flows.
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