Pages that link to "Item:Q1417666"
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The following pages link to Numerical investigation of unsteady transitional flows in turbomachinery components based on a RANS approach (Q1417666):
Displaying 9 items.
- Numerical solution of steady and unsteady transonic flow in turbine cascades and stages (Q597082) (← links)
- Modelling of unsteady transition in low-pressure turbine blade flows with two dynamic intermittency equations (Q608049) (← links)
- Numerical evaluation of turbulent flow structures in a stirred tank with a Rushton turbine based on scale-adaptive simulation (Q720938) (← links)
- Recent German research on periodical unsteady flow in turbomachinery (Q1041414) (← links)
- Characteristic regimes of transitional separation bubbles in unsteady flow (Q1417654) (← links)
- Prediction of turbine blade heat transfer and aerodynamics using a new unsteady boundary layer transition model (Q1599678) (← links)
- Prediction of the unsteady turbulent flow in an axial compressor stage. II: Analysis of unsteady RANS and LES data (Q1645478) (← links)
- Decomposition of the spatially filtered and ensemble averaged kinetic energy, the associated fluxes and scaling trends in a rotor wake (Q3557106) (← links)
- Revisiting RANS prediction of transitional flow on T3A flat plate subject to various freestream turbulences (Q6158470) (← links)
