Simulation of dynamical characteristics for complicated design scheme gas-turbine engines

Аuthors

Karasiov V. N.

Moscow Aviation Institute (National Research University), 4, Volokolamskoe shosse, Moscow, А-80, GSP-3, 125993, Russia

e-mail: aerospace@mai.ru

Abstract

Simulation dynamical models are discussed to analyze gas-turbine engines with complicated design layouts. These models are needed to study stability and control for airplanes with deflected thrust vector. Some examples are considered for dynamics of transition processes for integrated propulsion system based on double-flow turbojet engine with a separate fan.