Pages that link to "Item:Q929845"
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The following pages link to Numerical study of film cooled rotor leading edge with tip clearance in 1-1/2 turbine stage (Q929845):
Displaying 3 items.
- Investigation of influencing factors of hot streaks migration in high pressure stage of a vaneless counter-rotating turbine (Q1940778) (← links)
- Convective film cooling over a representative turbine blade leading-edge (Q1973119) (← links)
- Effect of incidence angle with wake passing on a film cooled leading edge: A numerical study (Q3579860) (← links)