Modeling of a face interface in a step of the axial compressor
DOI:
https://doi.org/10.15587/1729-4061.2010.2753Keywords:
model, experiment, the compressor, blade, flow, break-down, WBLs.Abstract
The engineering method of calculation of wall boundary layer in the axial-flow compressor, developed on the basis of the physical model of the flow gained as a result of numerical experiment by means of earlier tested on various plants 3-D of complex ANSYS CFX is reduced. The gained model allows to determine integral performances of wall flows on various operational modes, including and the conditions, previous a rotating stall.References
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