Algebraic grid generation for coolant passages of turbine blades with serpentine channels and pin fins
27th Joint Propulsion Conference ; 1991 ; Sacramento , CA , U.S.A.
01.01.1991
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
An Investigation of Coolant Within Serpentine Passages of a High-Pressure Axial Gas Turbine Blade
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