OPTIM generates profile of altitude, airspeed, and flightpath angle as function of range between given set or origin and destination points for particular models of transport aircraft. Profile is optimized in sense of minimizing fuel or time or in minimizing direct operating cost expressed as combination of fuel and time.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Vertical Profiles for Turbojet-Powered Aircraft


    Contributors:

    Published in:

    Publication date :

    1983-05-01



    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English


    Keywords :


    Measuring in-flight thrust of turbojet-powered aircraft

    Coleman, W.J. / DeSanto, D.F. | Engineering Index Backfile | 1958


    Noise levels of turbojet- and turbofan-powered aircraft

    Marsh, A.H. / McPike, A.L. | Engineering Index Backfile | 1963


    Deformable turbojet aircraft

    MA YUE / YAN XIAO / TANG MUCHENG et al. | European Patent Office | 2024

    Free access

    Aircraft turbojet nacelle

    FABRE CHRISTIAN / BIGNOLAIS ALAIN | European Patent Office | 2017

    Free access