Randomized trial demonstrates improved flow predictions in engineering applications, suggesting enhanced design accuracy.
Surface roughness significantly influences flow behavior across natural phenomena and engineering applications. Accurate prediction of these effects is essential for engineering design, yet modeling roughness-induced transition remains challenging due to the intricate interactions among surface roughness, boundary-layer development, and laminar separation. This study develops a novel machine-learning-enhanced [Formula: see text] transition model by introducing a transport equation for the roughness amplification factor [Formula: see text]. The key correction function associated with [Formula: see text] is explicitly derived using a multicase, computational-fluid-dynamics-driven machine-learning framework. The proposed model is assessed on canonical flat-plate boundary layers, airfoils, and turbine cascades under diverse flow conditions. Results demonstrate that the model effectively captures boundary-layer transition influenced by surface roughness and flow separation, achieving good agreement with both experimental and direct numerical simulation data. Further analysis reveals that [Formula: see text] plays a critical role in amplifying disturbances and promoting earlier transition onset. Overall, the present machine-learning framework provides a promising pathway for extending traditional RANS transition models to incorporate complex physical effects.
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Ge et al. (2026) studied this question.
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