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Stagnation region gas film cooling: Spanwise angled injection from multiple rows of holes. [gas turbine engines]
Stagnation region gas film cooling: Spanwise angled injection from multiple rows of holes. [gas turbine engines]
1981
D.W. Luckey
M. R. Lecuyer
Keywords:
Forced convection
Turbine blade
Stanton number
Classical mechanics
Stagnation point
Turbine
Physics
Aerospace engineering
gas turbines
fluid injection
Row
Mechanics
free flow
Correction
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