Cantilever monoplane, with 45-m. wing span; 2400 hp. developed by four Junkers L88 750-hp. engines; design is step toward flying wing; propellers, placed in front of leading edge by streamlined fairing receive power from engines by means of long transmission shafts; thickness of wing at socket exceeds 2 m. so that comfortable cabins can be arranged. (English description) (See also Aeronautique vol. 11, no. 127, Dec. 1929 p. 421, 3 figs; and Aero Digest, vol. 15, no. 6, Dec. 1929, p. 170, 1 fig.)


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    Titel :

    Tendency toward flying wing; the Junkers G38


    Weitere Titelangaben:

    Vers l'aile volante: le Junkers G 38


    Erschienen in:

    Flight ; 21 , n 48


    Erscheinungsdatum :

    1929


    Anmerkungen:

    3 Figs.


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Tendency toward flying wing; the Junkers G38

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