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

В статье исследуются вопросы диагностирования лопаток авиадвигателей в процессе эксплуатации на основе наборов значений спектров затухающих колебаний лопаток после ударного возбуждения. В ходе проведенных экспериментов предложен новый оператор мутации. // The article investigates issues of diagnosing blades of aircraft engines in operation basing on values sets of the spectra of damped oscillations of the blades after the shock excitation. In the series of the experiments a new mutation operator was suggested.