VERIFICATION OF MATHEMATIC MODELS OF A SMALL TURBOJET ENGINE MPM - 20

Abstract

Mathematical modeling is one of the most common ways of acquiring information and the properties of the object under examination. When changing the parameters entering the model can be obtained depending on the course and characteristics of the individual parts and the whole of subjects, which is the aviation turbojet engine MPM20. For this engine were created experimentally, graphical-analytical models and analytical a first level, whose analysis and verification is the goal of this post. Mathematical models of the engine are required to use its management, diagnostics and failure. Thanks analytical model and entering static characteristics, it is possible to calculate the parameters that are not measurable or difficult to measure.