Pages that link to "Item:Q1599678"
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The following pages link to Prediction of turbine blade heat transfer and aerodynamics using a new unsteady boundary layer transition model (Q1599678):
Displaying 9 items.
- Modelling of unsteady transition in low-pressure turbine blade flows with two dynamic intermittency equations (Q608049) (← links)
- The heat/mass transfer analogy for a simulated turbine blade (Q955546) (← links)
- Comparative analysis of steady state heat transfer in a TBC and functionally graded air cooled gas turbine blade (Q970117) (← links)
- Development and application of a novel technique for direct heat flux measurements in turbomachinery flows (Q1417659) (← links)
- On the importance of inlet boundary conditions for aerothermal predictions of turbine stages with large eddy simulation (Q1648371) (← links)
- On the use of entropy to predict boundary layer stability (Q1769760) (← links)
- Numerical simulation of steady-state heat transfer in a ceramic-coated gas turbine blade (Q1870742) (← links)
- Comparison of two unsteady intermittency models for bypass transition prediction on a turbine blade profile (Q1939038) (← 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)
