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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    Title :

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


    Contributors:

    Publication date :

    1989


    Size :

    11 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English