NASA, FAA, ONERA, and other partner organizations have embarked on a significant, collaborative research effort to address the technical challenges associated with icing on large scale, three-dimensional swept wings. These are extremely complex phenomena important to the design, certification and safe operation of small and large transport aircraft. There is increasing demand to balance trade-offs in aircraft efficiency, cost and noise that tend to compete directly with allowable performance degradations over an increasing range of icing conditions. Computational fluid dynamics codes have reached a level of maturity that they are being proposed by manufacturers for use in certification of aircraft for flight in icing. However, sufficient high-quality data to evaluate their performance on iced swept wings are not currently available in the public domain and significant knowledge gaps remain.


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    Titel :

    Initial Low-Reynolds Number Iced Aerodynamic Performance for CRM Wing


    Beteiligte:
    Woodard B. (Autor:in) / Diebold J. (Autor:in) / Broeren A. (Autor:in) / Potapczuk M. (Autor:in) / Lee S. (Autor:in) / Bragg M. (Autor:in)

    Erscheinungsdatum :

    2015


    Format / Umfang :

    23 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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