Forecasting of modes of rotating failure in a step of the axial compressor taking into account formation of profile and face interfaces
DOI:
https://doi.org/10.15587/1729-4061.2010.2786Keywords:
compressor, boundary layer, rotating stall, characteristics, experiment.Abstract
On the basis of variation principle of a maximum of stream of mechanical energy by the method of small indignations the criterion of transition of the axial compressor stage is developed to the modes of the revolved derangement, taking into account the features of forming type and butt-end boundary layers.References
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