Modeling of Highly Instrumented Honeywell Turbofan Engine Tested with Ice Crystal Ingestion in the NASA Propulsion System Laboratory
Author:
Affiliation:
1. NASA Glenn Research Center
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2016-3895
Reference14 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. 3Goodwin, R. V., Dischinger, D. G. "Turbofan Ice Crystal Rollback Investigation and Preparations Leading to Inaugural Ice Crystal Engine Test at NASA PSL-3 Test Facility," AIAA 2014-2895.
3. 4Oliver, M. J. "Validation Ice Crystal Icing Engine Test in the Propulsion Systems Laboratory at NASA Glenn Research Center," AIAA-2014-2898.
4. NASA Glenn Propulsion Systems Lab Ice Crystal Cloud Characterization Update 2015
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