Pages that link to "Item:Q1973119"
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The following pages link to Convective film cooling over a representative turbine blade leading-edge (Q1973119):
Displaying 13 items.
- Computational study of free-stream turbulence effects on film cooling using two different models (Q392862) (← links)
- Turbulent heat transfer and large coherent structures in trailing-edge cutback film cooling (Q431863) (← links)
- An experimental investigation of film cooling performance of louver scheme (Q533218) (← links)
- Discussions of some myths and concerned practices of film cooling research (Q547775) (← links)
- Numerical study of film cooled rotor leading edge with tip clearance in 1-1/2 turbine stage (Q929845) (← links)
- Mist film cooling simulation at gas turbine operating conditions (Q955559) (← links)
- A comparative study on showerhead cooling performance (Q981276) (← links)
- Shape optimization of a fan-shaped hole to enhance film-cooling effectiveness (Q992866) (← links)
- Heat transfer on a film-cooled rotating blade using different turbulence models (Q1973178) (← links)
- Calculation of the flow around a high-pressure turbine blade with cooling-jet injection from slots at the leading edge (Q1975851) (← links)
- Uncertainty quantification and film cooling (Q2362041) (← links)
- Effect of incidence angle with wake passing on a film cooled leading edge: A numerical study (Q3579860) (← links)
- Three-dimensional calculations of the flow field around a turbine blade with film cooling injection near the leading edge (Q5952018) (← links)