Two approaches to modeling turbofan engine component volume dynamics are explored and compared with a view toward application to real-time simulation of short take-off vertical landing (STOVL) aircraft propulsion systems. The first (and most popular) approach considers only heat and mass balances; the second approach includes a momentum balance and substitutes the heat equation with a complete energy balance. Results for a practical test case are presented and discussed.


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    Titel :

    STOVL (Short Take-Off Vertical Landing) Propulsion System Volume Dynamics Approximations


    Beteiligte:
    C. K. Drummond (Autor:in)

    Erscheinungsdatum :

    1989


    Format / Umfang :

    11 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch