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GlennICE 2.2 Capabilities and ResultsGlennICE (Glenn Icing Computational Environment) is a computational tool designed to calculate ice growth on complex three-dimensional geometries using the input from a user-supplied computational fluid dynamics (CFD) solution for the geometry of interest. The NASA John H. Glenn Research Center at Lewis Field is developing this tool to aid those evaluating, designing and certifying aircraft, engines, and aircraft components for flight in icing conditions. This domestically available software is being developed to enable the introduction of new icing physics into a computational environment in a manner that is open for evaluation and eventual use by industry, academia, and other government organizations. This paper will document the current capabilities for version 2.1 of this software and provide example cases with comparison to available experimental data.
Document ID
20220006386
Acquisition Source
Glenn Research Center
Document Type
Presentation
Authors
William Wright
(HX5, LLC)
David Rigby
(HX5, LLC)
Eric Galloway
(HX5, LLC)
Christopher Porter
(Glenn Research Center Cleveland, Ohio, United States)
Date Acquired
April 26, 2022
Subject Category
Aeronautics (General)
Meeting Information
Meeting: AIAA Aviation Forum and Exposition
Location: Chicago, IL
Country: US
Start Date: June 27, 2022
End Date: July 1, 2022
Sponsors: American Institute of Aeronautics and Astronautics
Funding Number(s)
WBS: 081876.02.03.15.01.04.01
CONTRACT_GRANT: 80GRC020D0003
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
Single Expert
Keywords
Icing
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