Method of calculating GTE gas-thermodynamic parameters with blade row description of an axial multistage compressor

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ژورنال

عنوان ژورنال: VESTNIK of the Samara State Aerospace University

سال: 2013

ISSN: 2541-7533,2542-0453

DOI: 10.18287/1998-6629-2013-0-3-2(41)-31-39