Improving the efficiency of axial compressors using control of the flow blades

Аuthors

Mitrofanov A. A.

Abstract

The article deals with activities that enable both theoretically and practically to improve the qualitative and quantitative characteristics of axial compressors, power plants, in particular, air-breathing jet engines. Based on the significant progress in the field of materials science and technology of complex-shaped parts, are invited to apply to the design of axial compressors known and suggested involving the authors methods of control flow around the blades (OPS). The results of theoretical and experimental research of the author on this issue received in the MAI.

Keywords:

сompressor blade, grating profiles, flow separation, control flow, a hollow blade, aerodynamic wake