THE JET-PROPELLED AERO-ENGINE EXHAUST ARRANGEMENT

Abstract

The article tries to approach the issue of system output, first in terms of distribution and description of the output system, then in terms of temperature control gas output in these systems and also describes a specific set of output engine RD-33rd. Finally a static model developed in the MATLAB environment presents the program of section change nozzles depending on the position of TL. Materials to final processing have been collected from various sources from leading DT, the TU library, teachers at FA and websites.