Selection efficient control algorithms of fuel-air solution by complex of staff-measured factors
Aerospace propulsion engineering
AbstractThe authors has been viewed method of getting ultimate air excess factor by staff - measured engine operation factors which are taken into consideration engines unit performance degradation, during its operation. In this article is shown comparative analysis of turbo - jet engines management efficiency of afterburning conditions between traditional, program control and proposal.
Keywords:afterburning combastion chamber, staff-mesuared parameters, coefficient of summary air surplus, controlling law algorithm of calculation, regression model