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.
author list (cited authors)
Schobeiri, M. T., & Attia, M. S.