Performance Analysis of a Compressor Leading Edge without Pressure Spike at High Subsonic Speed
نویسندگان
چکیده
منابع مشابه
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ژورنال
عنوان ژورنال: International Journal of Gas Turbine, Propulsion and Power Systems
سال: 2020
ISSN: 1882-5079
DOI: 10.38036/jgpp.11.4_56