A computational method for dynamic simulation of aero- and stationary gas turbine engines
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In this paper a new computational method for accurate simulation of the nonlinear dynamic behavior of single- and multi-spool core engines, turbofan engines and power generation gas turbine engines is presented. To perform simulation, a modularly structured computer code has been developed which includes individual mathematical modules representing various engine components. To demonstrate the versatility of the method, several critical simulation cases are presented.