Increases in aircraft and engine performance are increasing the heat load being transferred into an aircraft's primary coolant--the fuel. This research is aimed at understanding the limitations of operation of fuel heated to 48 deg C (90 deg F) and beyond. Important issues are expected to be thermal stability, heat transfer/flow instabilities, and injection/combustion properties.


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    Titel :

    Advanced Supercritical Fuels


    Beteiligte:
    T. Edwards (Autor:in) / J. Gord (Autor:in) / C. Bunker (Autor:in)

    Erscheinungsdatum :

    2001


    Format / Umfang :

    4 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





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