Propulsion and Power Plants
Аuthors
Moscow Aviation Institute (National Research University), 4, Volokolamskoe shosse, Moscow, А-80, GSP-3, 125993, Russia
e-mail: yuri_zuev@bk.ru
Abstract
Some theoretical results are discussed concening to two-phase flows in nozzles and streams used to lay coatings by means of a gas-dynamical technique. An approach is offered to calculate sequentally properties of these flows. The approach enables to select a sort and parameters of gas, as well as geometry for the nozzle. Furthermore a size of a coating region is predicted depending on distance between the nozzle and a processed component surface.
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