Modeling of Commercial Turbofan Engine with Ice Crystal Ingestion; Follow-On
Author:
Affiliation:
1. NASA Glenn Research Center
2. Kent State University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2014-2899
Reference13 articles.
1. 1Mason, J. G., Chow, P., Fuleki, D. M. "Understanding Ice Crystal Accretion and Shedding Phenomenon in Jet Engines Using a Rig Test," GT2010-22550.
2. 3Veres, J. P., Jorgenson, P. C. E. "Modeling Commercial Turbofan Engine Icing Risk with Ice Crystal Ingestion", AIAA 2013-2679.
3. 4Veres, J. P., Jorgenson, P. C. E., Wright, W. B., Struk, P. "A Model to Assess the Risk of Ice Accretion due to Ice Crystal Ingestion in a Turbofan Engine and its Effects on Performance", AIAA 2012-3038.
4. Engine Icing Modeling and Simulation (Part I): Ice Crystal Accretion on Compression System Components and Modeling its Effects on Engine Performance
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1. Numerical Investigation of Particle Breakup and Ingestion into an Axial Low Pressure Compressor at Engine Icing Operating Points;2018 Atmospheric and Space Environments Conference;2018-06-24
2. Viscous Three Dimensional Simulation of Flow in an Axial Low Pressure Compressor at Engine Icing Operating Points;9th AIAA Atmospheric and Space Environments Conference;2017-06-02
3. Modeling the Deterioration of Engine and Low Pressure Compressor Performance During a Rollback Event due to Ice Accretion;50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference;2014-07-25
4. Turbofan Ice Crystal Rollback Investigation and Preparations Leading to Inaugural Ice Crystal Engine Test at NASA PSL-3 test Facility;6th AIAA Atmospheric and Space Environments Conference;2014-06-13
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