Pages that link to "Item:Q1939038"
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The following pages link to Comparison of two unsteady intermittency models for bypass transition prediction on a turbine blade profile (Q1939038):
Displaying 4 items.
- Modelling of unsteady transition in low-pressure turbine blade flows with two dynamic intermittency equations (Q608049) (← links)
- Further development of a dynamic intermittency model for wake-induced transition (Q1041422) (← links)
- Prediction of turbine blade heat transfer and aerodynamics using a new unsteady boundary layer transition model (Q1599678) (← links)
- Study of modeling unsteady blade row interaction in a transonic compressor stage. II: Influence of deterministic correlations on time-averaged flow prediction (Q2451582) (← links)