Expressions developed for max range for three cruise flight conditions: constant altitude, varying altitude below 35,000 ft, and varying altitude above 35,000 ft; max range obtained by increasing cruising altitude as fuel is consumed; airplane configurations derived which correspond to aerodynamic optima for cruise conditions investigated; importance of thrust loading. (See also - discussion n 6 June p 341-2)


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    Titel :

    Range performance of turbojet airplanes


    Weitere Titelangaben:

    J Aeronautical Sciences


    Beteiligte:
    Ashkenas, I.L. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1948


    Format / Umfang :

    5 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :





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