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.


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    Titel :

    Introduction to the Glenn Icing Computational Environment (GlennICE)


    Beteiligte:
    T. Ozoroski (Autor:in)

    Erscheinungsdatum :

    2024


    Format / Umfang :

    64 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





    Mixed Phase Modeling in GlennICE with Application to Engine Icing

    Wright, William / Jorgenson, Phil / Veres, Joseph | AIAA | 2010


    Scalability of GlennICE in a Parallel Environment

    Porter, Christopher / Sabri, Zaid | SAE Technical Papers | 2023


    Scalability of GlennICE in a Parallel Environment

    Sabri, Zaid / Porter, Christopher | British Library Conference Proceedings | 2023


    GlennICE Manual 4.1.0

    C. Porter / M. Potapczuk / T. Ozoroski et al. | NTIS | 2024