Development and Turbine Engine Performance of Three Advanced Rhenium Containing Superalloys for Single Crystal and Directionally Solidified Blades and Vanes (97-GT-117)
1998
Aufsatz (Zeitschrift)
Englisch
Creep-Fatigue Tests on Full Scale Directionally Solidified Turbine Blades
Online Contents | 2008
|Cooling Modern Aero Engine Turbine Blades and Vanes
SAE Technical Papers | 1966
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