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.
В.А. Коваль, Е.А. Ковалева Modeling of a face interface in a step of the axial compressor // Східно-Європейський журнал передових технологій, Vol. 3, Issue 2, 2012, pp. 20-24