Abstract
The way of the solution of increasing effectivity gas turbine engine problem is considered. Results of researches of the axial compressor stage with constant circulation are submitted. Recommendations for profiling two-row blade rings are developed on the basis of use of ejection effect with mixing flow ejected gas and gas ejected in semibounded space. Comparative analysis of results of experimental research of two-row blade rings and one-row blade rings has been done. Recommendations for use gas turbine engine axial compressor stage profiled according to the law of constant circulation with small values of hub ratio are carried out.
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