Turbofan Engine Post-Instability Behavior - Computer Simulations, Test Validation, and Application of Simulations,
GENERAL ELECTRIC CO EVENDALE OH AIRCRAFT ENGINE GROUP
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This paper presents a method that can be used to predict the post-stability operation of a turbofan engine and is based upon extending the capabilities of engine transient cycle decks. Typical predictions are presented and compared with results obtained from the testing of a modern augmented turbofan engine. The potential manners in which this new digital-computer-simulation tool may be used are also discussed.
- Fluid Mechanics
- Jet and Gas Turbine Engines