Boundary-layer transition prediction using a simplified correlation-based model
Xia Chenchao - Zhejiang University
(in lingua inglese)
The new transition model is implemented into an inhouse CFD solver and tested for some typical cases, ranging from low speed flows to hypersonic flows. Results from simulations in this work show that the accuracies of the flows are significantly improved by the proposed transition model, compared with the fully laminar and fully turbulent calculations.
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Fonte: Articolo Chinese Journal of Aeronautics, 2015
Settori: Fluidodinamica, Software di simulazione
Parole chiave: CFD
- Alessio Castorrini
- Roberta De Robbio