Optimization of A Swirl with Impingement Compound Cooling Unit for A Gas Turbine Blade Leading Edge
نویسندگان
چکیده
منابع مشابه
Simulating Cooling Injection Effect of Trailing Edge of Gas Turbine Blade on Surface Mach Number Distribution of Blade
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ژورنال
عنوان ژورنال: Energies
سال: 2020
ISSN: 1996-1073
DOI: 10.3390/en13010210