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Simulating Ice Accretion Effects on Engine PerformanceDevelop a modeling tool that can be used to predict the onset of engine icing due to ice crystal ingestion. The tool will be capable of modeling the effects of ice build up as well as its effect on engine performance. Perform a parametric study of an engine with simulated ice blockage effects at altitude conditions. Using the tool, estimate the effect of blockage in the low pressure compressor due to ice buildup (accretion), and its effects on engine performance.
Document ID
20150010145
Acquisition Source
Glenn Research Center
Document Type
Presentation
Authors
Jorgenson, Philip C. E. (NASA Glenn Research Center Cleveland, OH, United States)
Veres, Joseph P. (NASA Glenn Research Center Cleveland, OH, United States)
Wright, William (NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
June 8, 2015
Publication Date
May 10, 2011
Subject Category
Air Transportation And Safety
Aircraft Design, Testing And Performance
Report/Patent Number
E-667816
Report Number: E-667816
Meeting Information
Meeting: Aviation Safety Program Annual Technical Meeting
Location: St. Louis, MO
Country: United States
Start Date: May 10, 2011
End Date: May 12, 2011
Sponsors: NASA Glenn Research Center
Funding Number(s)
WBS: WBS 648987.02.01.03.10
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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