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JOURNALS // Prikladnaya Mekhanika i Tekhnicheskaya Fizika // Archive

Prikl. Mekh. Tekh. Fiz., 2015 Volume 56, Issue 2, Pages 21–31 (Mi pmtf961)

Investigation of the effect of roughness of duct surfaces of a supersonic high-pressure stage of an axial compressor on its characteristics

A. A. Inozemtsev, A. I. Plotnikov

Open Joint-Stock Company "Aviadvigatel", Perm’, 614990, Russia

Abstract: Results of calculations and experimental investigations of characteristics of a supersonic high-pressure wide-chord stage of an axial compressor are presented. The influence of surface roughness on the characteristics of this stage are analyzed. A method of identification of aerodynamic flow parameters in the compressor duct is described.

Keywords: axial compressor, high-pressure wide-chord stage, three-dimensional calculation, stable operation, equivalent surface roughness, identification, compressor characteristic.

UDC: 621.51

DOI: 10.15372/PMTF20150203


 English version:
Journal of Applied Mechanics and Technical Physics, 2015, 56:2, 182–191

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