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Introduction to the Glenn Icing Computational Environment (GlennICE)The NASA John H. Glenn Research Center at Lewis Field is developing the Glenn Icing Computational Environment (GlennICE) tool to aid those evaluating, designing and certifying aircraft, engines, and aircraft components for flight in icing conditions. This short course will walk through some of the underlying physics involved with GlennICE and how we achieve efficient 3D ice accretion predictions. After an introduction of GlennICE, an analysis of the Common Research Model High-Lift will be demonstrated to showcase the typical workflow for an aircraft icing analysis. Within this walkthrough, capabilities will be highlighted with future planned capabilities being discussed. Finally, we will showcase the impact GlennICE is having on NASA’s icing portfolio and how it is advancing aircraft icing research and safety.
Document ID
20240010795
Acquisition Source
Glenn Research Center
Document Type
Presentation
Authors
Thomas Ozoroski
(Glenn Research Center Cleveland, United States)
Date Acquired
August 20, 2024
Subject Category
Aircraft Design, Testing and Performance
Meeting Information
Meeting: Thermal and Fluids Analysis Workshop (TFAWS)
Location: Cleveland, OH
Country: US
Start Date: August 26, 2024
End Date: August 30, 2024
Sponsors: Glenn Research Center
Funding Number(s)
WBS: 109492.02.03.09.09
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Technical Review
Single Expert
Keywords
Icing
GlennICE
Computational Icing
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