The aircraft energy-climb trajectory for configurations with a sharp transonic drag rise is well known to possess two branches in the altitude/Mach-number plane. Transition in altitude between the two branches occurs instantaneously, a 'corner' in the minimum-time solution obtained with the energy-state model. If the initial and final values of altitude do not lie on the energy-climb trajectory, then additional jumps (crude approximations to dives and zooms) are required at the initialand terminal points. With a singular-perturbation approach, a 'boundary-layer' correction is obtained for each altitude jump, the transonic jump being a so-called 'internal' boundary layer, different in character from the initial and terminal layers. The determination of this internal boundary layer is examined and some computational results for an example presented.


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    Titel :

    Altitude transitions in energy climbs


    Weitere Titelangaben:

    Hoehenuebergaenge und Energiezunahme bei Hochgeschwindigkeitsfluegen


    Beteiligte:
    Weston, A.R. (Autor:in) / Cliff, E.M. (Autor:in) / Kelley, H.J. (Autor:in)

    Erschienen in:

    Automatica, Oxford ; 19 , 2 ; 199-202


    Erscheinungsdatum :

    1983


    Format / Umfang :

    4 Seiten, 4 Bilder, 12 Quellen



    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch




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