Model operation of electrolyte in the spark gap at the electrochemical working compressor blades with using method of final elements in the software environment “FLUENT”

Abstract

The article is devoted to the actual problem of the up-to-date aviation propulsion engineering – the raising of form accuracy at the electrochemical working. In the article the results of the development work with respect to creation methodology of model operation of electrolyte current in the spark gap are presented. Proper models are submitted. Areas of use of results of work are discussed.