GlennICE (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.
GlennICE 2.2 Capabilities and Results
AIAA Aviation, American Institute of Aeronautics and Astronautics ; 2022 ; Chicago, IL, US
Aufsatz (Konferenz)
Keine Angabe
Englisch
GlennICE 2.1 Capabilities and Results
AIAA | 2022
|Scalability of GlennICE in a Parallel Environment
SAE Technical Papers | 2023
|Scalability of GlennICE in a Parallel Environment
British Library Conference Proceedings | 2023
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