The work summarized in this report is a continuation of NASA's Large-Scale, Swept-Wing Test Articles Fabrication; Research and Test Support for NASA IRT contract (NNC10BA05 -NNC14TA36T) performed by Boeing under the NASA Research and Technology for Aerospace Propulsion Systems (RTAPS) contract. In the study conducted under RTAPS, a series of icing tests in the Icing Research Tunnel (IRT) have been conducted to characterize ice formations on large-scale swept wings representative of modern commercial transport airplanes. The outcome of that campaign was a large database of ice-accretion geometries that can be used for subsequent aerodynamic evaluation in other experimental facilities and for validation of ice-accretion prediction codes.


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    Titel :

    Icing Simulation Research Supporting the Ice-Accretion Testing of Large-Scale Swept-Wing Models


    Beteiligte:
    Yadlin, Yoram (Autor:in) / Monnig, Jaime T. (Autor:in) / Malone, Adam M. (Autor:in) / Paul, Bernard P. (Autor:in)

    Erscheinungsdatum :

    2018-03-01


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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