Aerodynamic Optimization Design of a Supersonic Compressor Rotor with High Pressure Ratio
نویسندگان
چکیده
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ژورنال
عنوان ژورنال: International Journal of Aerospace Engineering
سال: 2021
ISSN: 1687-5974,1687-5966
DOI: 10.1155/2021/6664968