Discussion of question of performance and factors on which it depends, in order to justify numerical values given; if airplane can be produced, with gliding angle as low as 1 in 25, to "take-off" and fly at low altitude carrying half its gross weight in fuel, there is every prospect that half-circumference of earth, 12, 600 mi, may be covered in single flight without refueling. (See also - n 3840 Aug 18 1939 p 203-5)


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    Titel :

    Maximum range of flight


    Weitere Titelangaben:

    Engineering


    Beteiligte:

    Erschienen in:

    Engineering ; 148 , n 3841


    Erscheinungsdatum :

    1939


    Format / Umfang :

    3 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch




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