Rotorcraft Engine Contingency Power Requirements and the Need for More Accurate Turbine Blade Lifing Methodologies
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- SKU # : 57-00137
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Rotorcraft Engine Contingency Power Requirements and the Need for More Accurate Turbine Blade Lifing Methodologies
Authors / Details: Samuel D. Spring, GE Aircraft Engines; Martin M. D?Angelo, GE Aircraft Engines; Kevin S. O?Hara, GE Aircraft EnginesRecently Viewed Items
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