Control Design for an Advanced Geared Turbofan Engine
Author:
Affiliation:
1. NASA Glenn Research Center
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2017-4820
Reference15 articles.
1. A Modular Aero-Propulsion System Simulation of a Large Commercial Aircraft Engine
2. Control Design for a Generic Commercial Aircraft Engine
3. Dynamic Analysis for a Geared Turbofan Engine with Variable Area Fan Nozzle
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