Pages that link to "Item:Q1975851"
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The following pages link to Calculation of the flow around a high-pressure turbine blade with cooling-jet injection from slots at the leading edge (Q1975851):
Displaying 5 items.
- Numerical simulation on the effect of jet nozzle position on impingement cooling of gas turbine blade leading edge (Q646588) (← links)
- A comparative study on showerhead cooling performance (Q981276) (← 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)
- Numerical investigation of the aerodynamics of the near-slot film cooling. (Q4943448) (← links)
- Three-dimensional calculations of the flow field around a turbine blade with film cooling injection near the leading edge (Q5952018) (← links)