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. (see also English description in Flight, vol. 21, no. 48, Nov. 29, 1929, p. 1264, 3 figs.; and Aero Digest, vol. 15, no. 6, Dec. 1929, p. 170, 1 fig.)


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Tendency toward flying wing; the Junkers G38


    Weitere Titelangaben:

    Vers l'aile volante: le Junkers G 38


    Erschienen in:

    Aeronautique ; 11 , n 127


    Erscheinungsdatum :

    1929


    Anmerkungen:

    3 Figs.


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Französisch


    Schlagwörter :


    Tendency toward flying wing; the Junkers G38

    Engineering Index Backfile | 1929


    Tendency toward flying wing; the Junkers G38

    Engineering Index Backfile | 1929


    Modern junkers wing

    Quick, A.W. | Engineering Index Backfile | 1937


    Junkers double wing

    Billeb, E. | Engineering Index Backfile | 1935


    The Modern Junkers Wing

    Quick, A.W. | Emerald Group Publishing | 1937