Pages that link to "Item:Q5952018"
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The following pages link to Three-dimensional calculations of the flow field around a turbine blade with film cooling injection near the leading edge (Q5952018):
Displaying 6 items.
- Numerical simulation on the effect of jet nozzle position on impingement cooling of gas turbine blade leading edge (Q646588) (← links)
- Application of the TLVA model for predicting film cooling under rotating frames (Q992870) (← links)
- Investigation of density ratio effects on normally injected cold jets into a hot cross flow (Q1020353) (← links)
- Calculation of the flow around a high-pressure turbine blade with cooling-jet injection from slots at the leading edge (Q1975851) (← links)
- Application of an unstructured Navier-Stokes code to prediction of adiabatic effectiveness of endwall flush-slot-cooling for a stator vane passage (Q2483321) (← links)
- Effect of incidence angle with wake passing on a film cooled leading edge: A numerical study (Q3579860) (← links)