What is it about?
Modeling of a turbofan engine with a thermodynamic cycle code, and an Euler based compressor flow analysis code, to identify key icing parameters that are the precursors to ice accretion in a turbofan engine.
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Why is it important?
Wet bulb temperature at the location where there is ice accretion within the low pressure compressor of a turbofan engine.
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This page is a summary of: Performance Modeling of Honeywell Turbofan Engine Tested with Ice Crystal Ingestion in the NASA Propulsion System Laboratory, June 2015, SAE International,
DOI: 10.4271/2015-01-2133.
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