Aerodynamic Approach to the Design of Blade Profiles Suitable for Compressor Cascade : 2nd Report, Inverse Boundary Layer Theoryand Blade Design Method

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ژورنال

عنوان ژورنال: TRANSACTIONS OF THE JAPAN SOCIETY OF MECHANICAL ENGINEERS Series B

سال: 1983

ISSN: 0387-5016,1884-8346

DOI: 10.1299/kikaib.49.2292