Design and Strength Analysis of Curved-Root Concept for Compressor Rotor Blade in Gas Turbine
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چکیده
منابع مشابه
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ژورنال
عنوان ژورنال: Fatigue of Aircraft Structures
سال: 2017
ISSN: 2300-7591
DOI: 10.1515/fas-2017-0011